DOE-HDBK-1010-92, Classical Physics

DOE-HDBK-1010-92 JUNE 1992 DOE FUNDAMENTALS HANDBOOK CLASSICAL PHYSICS U.S. Department of Energy FSC-6910 Washington, D.C. 20585 Distribution Statement A. Approved for public release; distribution is unlimited. WELCOME This Portable Document Format (PDF) file contains bookmarks, thumbnails, and hyperlinks to help you navigate through the document. All items listed in the Overview are linked to the corresponding sections. In addition, if you click on a heading while you are reading the text, you will return to the Table of Contents for that section. Click on the DOE seal below to move to the Overview page. This document has been reproduced directly from the best available copy. Available to DOE and DOE contractors from the Office of Scientific and Technical Information. P. O. Box 62, Oak Ridge, TN 37831; (615) 576-8401. Available to the public from the National Technical Information Service, U.S. Department of Commerce, 5285 Port Royal Rd., Springfield, VA 22161. Order No. DE92019784 CLASSICAL PHYSICS Rev. 0 CP ABSTRACT The Classical Physics Fundamentals Handbook was developed to assist nuclear facility operating contractors provide operators, maintenance personnel, and the technical staff with the necessary fundamentals training to ensure a basic understanding of physical forces and their properties. The handbook includes information on the units used to measure physical properties; vectors, and how they are used to show the net effect of various forces; Newton's Laws of motion, and how to use these laws in force and motion applications; and the concepts of energy, work, and power, and how to measure and calculate the energy involved in various applications. This information will provide personnel with a foundation for understanding the basic operation of various types of DOE nuclear facility systems and equipment. Key Words: Training Material, Classical Physics, Vectors, Newton's Laws, Energy, Work, Power CLASSICAL PHYSICS Rev. 0 CP FOREWORD The Department of Energy (DOE) Fundamentals Handbooks consist of ten academic subjects, which include Mathematics; Classical Physics; Thermodynamics, Heat Transfer, and Fluid Flow; Instrumentation and Control; Electrical Science; Material Science; Mechanical Science; Chemistry; Engineering Symbology, Prints, and Drawings; and Nuclear Physics and Reactor Theory. The handbooks are provided as an aid to DOE nuclear facility contractors. These handbooks were first published as Reactor Operator Fundamentals Manuals in 1985 for use by DOE Category A reactors. The subject areas, subject matter content, and level of detail of the Reactor Operator Fundamentals Manuals was determined from several sources. DOE Category A reactor training managers determined which materials should be included, and served as a primary reference in the initial development phase. Training guidelines from the commercial nuclear power industry, results of job and task analyses, and independent input from contractors and operations-oriented personnel were all considered and included to some degree in developing the text material and learning objectives.

The DOE Fundamentals Handbooks represent the needs of various DOE nuclear facilities' fundamentals training requirements. To increase their applicability to nonreactor nuclear facilities, the Reactor Operator Fundamentals Manual learning objectives were distributed to the Nuclear Facility Training Coordination Program Steering Committee for review and comment. To update their reactor-specific content, DOE Category A reactor training managers also reviewed and commented on the content. On the basis of feedback from these sources, information that applied to two or more DOE nuclear facilities was considered generic and was included. The final draft of each of these handbooks was then reviewed by these two groups. This approach has resulted in revised modular handbooks that contain sufficient detail such that each facility may adjust the content to fit their specific needs. Each handbook contains an abstract, a foreword, an overview, learning objectives, and text material, and is divided into modules so that content and order may be modified by individual DOE contractors to suit their specific training needs. Each subject area is supported by a separate examination bank with an answer key. The DOE Fundamentals Handbooks have been prepared for the Assistant Secretary for Nuclear Energy, Office of Nuclear Safety Policy and Standards, by the DOE Training Coordination Program. This program is managed by EG&G Idaho, Inc. CLASSICAL PHYSICS Rev. 0 CP OVERVIEW TheDepartment of Energy Fundamentals HandbookentitledClassical Physicswas prepared as an information resource for personnel who are responsible for the operation of the Department's nuclear facilities. A basicunderstanding of classicalphysics is necessary for DOE nuclearfacility operators, maintenance personnel, and the technical staff tosafelyoperate andmaintain the facility and facility support systems. The information in thehandbook is presented to provide a foundation for applying engineeringconcepts to the job.This knowledgewill help personnel morefully understand the impactthat their actions may have on the safe andreliableoperation offacility components and systems. TheClassical Physicshandbook consists offive modulesthat arecontained in one volume. The following is a briefdescription of the information presented in each module of the handbook. Module 1 - Unit Systems This modulepresents the concept ofunit systems for the fundamental dimensions of mass, length, and time used in physics. Additionally, derivation of units and the conversion of these units is presented. Module 2 - Vectors This module contains information to aid in the determination of the net effect of various forces on an object andincludes graphingvectors,adding vectors, anddetermining component vectors of a resultant vector. Module 3 - Force and Motion This modulepresents Newton's Laws of force and motion. Module 4 - Application of Newton's Laws This module describes the effect of static anddynamicforces on objects andincludes a discussion of the forcescommonlyencountered in a nuclearfacility. Module 5 - Energy, Work, and Power This module definesenergy,work, and power,identifies theirvarious forms, and discusses the conservation of energy,work, and powerincluding themeasurement and calculation of each. CLASSICAL PHYSICS Rev. 0 CP The information contained in this handbook is by no means all encompassing. Anattempt to present the entirescience of classical physicswould be impractical.However, theClassical

Physicshandbook does present enoughinformation to provide thereaderwith a fundamental knowledgelevel sufficient tounderstand the advanced theoretical concepts presented inother subject areas, and tobetter understandbasic system and equipmentoperations. Department of Energy Fundamentals Handbook CLASSICAL PHYSICS Module 1 Unit Systems Unit System TABLE OF CONTENTS Rev.0 CP-01Page i TABLE OF CONTENTS LIST OF FIGURES. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ii LIST OF TABLES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . iii REFERENCES. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . iv OBJECTIVES. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . v FUNDAMENTAL DIMENSIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 Fundamental Dimensions. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 Units . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 Unit Systems. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 Derived Measurements. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6 Summary. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8 UNIT CONVERSIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9 Conversion Factors. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9 Unit Conversion. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10 Steps forUnit Conversion . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11 Summary. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16 LIST OF FIGURES Unit Systems CP-01 Rev. 0Page ii LIST OF FIGURES NONE Unit Systems LIST OF TABLES Rev.0 CP-01Page iii LIST OF TABLES Table 1 English Units ofMeasurement. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 Table 2 MKS Units ofMeasurement. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 Table 3 CGS Units ofMeasurement. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 Table 4 Approximate Length ofFamiliarObjects . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5 Table 5 Approximate Masses ofFamiliarObjects. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5 Table 6 Approximate Times of FamiliarEvents . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6 Table 7 Conversion Table. .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10 Table 8 Conversion Factors. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14 REFERENCES Unit Systems CP-01 Rev. 0Page iv REFERENCES C Beiser, Arthur,Applied Physics Schaums Outline Series, McGraw-Hill Book Company, 1976.

C Murray, Raymond andCobb, Grover,Physics Concepts and Consequences, Prentice-Hall, Inc., 1970. C Alexander, Joseph, et al.,Physics for Engineering Technology, John Wiley and Sons, 1978. C Sears,Francis and Zemansky,Mark, University Physics, 3rd edition, Addison- Wesley Publishing Co. C Science and Fundamental Engineering(SAFE), Classical Physics, "Measure" Windsor, CT: Combustion Engineering,Inc., 1988. C Academic Program for Nuclear Power Plant Personnel, Volume II, General Physics Corporation, Library of Congress Card #A 397747,April 1982. Unit Systems OBJECTIVES Rev.0 CP-01Page v TERMINAL OBJECTIVE 1.0 Given appropriate conversion tables,CONVERT betweenEnglish and SI system units of measurement. ENABLING OBJECTIVES 1.1 DEFINE the threefundamental dimensions: length, mass, and time. 1.2 LIST standard units of thefundamental dimensions for each of the following systems: a. International System of Units(SI) b. English System 1.3 DIFFERENTIATE between fundamental and derived measurements. 1.4 Given appropriate conversion tables,CONVERT betweenEnglish and SI units oflength. 1.5 Givenappropriate conversion tables,CONVERT betweenEnglish and SI units of mass. 1.6 CONVERT time measurementsbetween the following: a. Years b. Weeks c. Days d. Hours e. Minutes f. Seconds Unit Systems CP-01 Rev. 0Page vi Intentionally Left Blank Unit Systems FUNDAMENTAL DIMENSIONS Rev. 0 Page 1 CP-01 FUNDAMENTAL DIMENSIONS Length, mass, and time are the three fundamental dimensions onwhich the measurement of all physical quantities is dependent. EO 1.1 DEFINE the three fundamental dimensions: length, mass, and time. EO 1.2 LIST standard units of the fundamentaldimensions for each of the following systems: a. International System of Units (SI) b. English System EO 1.3 DIFFERENTIATE between fundamental and derived measurements. Fundamental Dimensions Physics is a science based upon exact measurement ofphysicalquantitiesthat are dependent upon three fundamental dimensions. The three fundamental or primary dimensions aremass, length,and time. These threefundamental units must beunderstood in order to lay the foundation for the manyconcepts andprinciples presented in this material. Mass Massis the amount of material present in an object. This measurement describes "how much" material makes up an object. Often, mass andweight are confused asbeing the same because theunits used to describe them aresimilar. Weight (a derived unit, not a fundamental unit) is a measurement thatdescribes the force of gravity on the "mass" of an object. Length Lengthis the distance between two points. The concept oflength is needed to locate the position of a point in space and thereby describe thesize of a physicalobject or system. When measuring a length of pipe, the ends of the pipe are the two points and the distance between the two points is the length. Atypical unit used to describe length is the"foot." FUNDAMENTAL DIMENSIONS Unit Systems CP-01 Page 2 Rev. 0 Time Timeis the duration between two instants. The measurement oftime is described in units of seconds, minutes, orhours. Units A number alone is not sufficient to describe aphysicalquantity. For example, to saythat "a pipe must be 4 long to fit" has no meaning unless a unit ofmeasurement for length is also specified. By adding units to the number, it becomes clear, "a pipe must be 4 feet long to fit."

The unit defines the magnitude of ameasurement. If we have a measurement of length, the unit used to describe the length could be afoot or yard, each ofwhich describes a different magnitude of length. The importance ofspecifying the units of ameasurement for a number used to describe aphysicalquantity is doubly emphasized when it is notedthat the same physical quantity may be measured using a variety of different units. For example, length may be measured in meters, inches, miles, furlongs, fathoms, kilometers, or a variety ofotherunits. Units of measurement have been established for use with each of the fundamental dimensions mentioned previously. The following section describes the unit systems in usetoday and providesexamples of unitsthat are used ineach system. Unit Systems There are two unit systems in use at thepresenttime, English units andInternational System of Units (SI). In the United States, the English system is currentlyused. This systemconsists of various units for each of the fundamental dimensions or measurements. These units are shown in Table 1. Unit Systems FUNDAMENTAL DIMENSIONS Rev. 0 Page 3 CP-01 TABLE 1 English Units of Measurement Length Mass Time Inch Ounce *Second * Foot * Pound Minute Yard Ton Hour Mile Day Month Year * Standardunit of measure The English system is presentlyused in thefield of engineering andthroughout the United States. The foot-pound-second (FPS)system is the usual unit systemused in the U.S. when dealing with physics. Over the years therehave been movements tostandardize units sothat all countries,including the United States,will adopt the SIsystem. The SI system is made up of two related systems, the meter-kilogram-second (MKS)system and thecentimeter-gram-second (CGS)system. The MKS and CGS systems are much simpler to usethan theEnglish systembecause they use a decimal-based system in which prefixes areused to denote powers of ten. Forexample, one kilometer is 1000 meters, and one centimeter is one one-hundredth of a meter. TheEnglish system has odd units of conversion. For example, amile is 5280 feet, and aninch is onetwelfth of a foot. FUNDAMENTAL DIMENSIONS Unit Systems CP-01 Page 4 Rev. 0 The MKS system isusedprimarily for calculations in thefield of physics whileboth the MKS and CGS systems areused in thefield of chemistry. Theunits for each of these systems are shown in Tables 2 and 3 below. TABLE 2 MKS Units of Measurement Length Mass Time Millimeter Milligram * Second * Meter Gram Minute Kilometer * Kilogram Hour Day Month Year * Standardunit of measure TABLE 3 CGS Units of Measurement Length Mass Time * Centimeter Milligram * Second Meter * Gram Minute Kilometer Kilogram Hour Day Month Year * Standardunit of measure Unit Systems FUNDAMENTAL DIMENSIONS Rev. 0 Page 5 CP-01 The following tables show approximate lengths, masses, andtimes for somefamiliar objects or events. TABLE 4 Approximate Lengths of Familiar Objects Object Length (meters) Diameter of Earth Orbit Around Sun 2 x 10 FootballField 1 x 10 Diameter ofDime 2 x 10 Thickness of Window Pane 1 x 10 Thickness ofPaper 1 x 10 11 2 -2 -3 -4 TABLE 5 Approximate Masses of Familiar Objects Object Mass (kilograms) Earth 6 x 10 House 2 x 10 Car 2 x 10 Quart of Water 1 Dime 3 x 10 Postage Stamp 5 x 10 24 5 3 -3 -8 FUNDAMENTAL DIMENSIONS Unit Systems CP-01 Page 6 Rev. 0 TABLE 6 Approximate Times of Familiar Events Event Time (seconds)

Age of Earth 2 x 10 HumanLife Span 2 x 10 Earth Rotation Around Sun 3 x 10 Earth Rotation AroundAxis 8.64 x 10 Time Between Heart Beats 1 17 9 7 4 Derived Measurements Most physical quantities have unitsthat arecombinations of thethreefundamentaldimensions of length, mass, and time. When these dimensions or measurements are combined, theyproduce what are referred to asderivedunits. This meansthat they have been "derived" from one or more fundamental measurements. These combinations of fundamental measurements can be the combination of the same or different units. The following are examples ofvarious derived units. Ar ea Area is the product of two lengths (e.g., width xlength for a rectangle);thus, it has the units of lengthsquared, such as squareinches (in. ) orsquare meters (m ).2 2 1 m x 1 m = 1 m2 4 in. x 2 in. = 8 in.2 Volume Volume is the product of three lengths (e.g.,length x width xdepth for a rectangular solid); thus, it has the units of length cubed, such as cubic inches (in. ) or cubicmeters3 (m ). The MKS and CGS unit systems have a specific unit for volume called the liter3 (l). One liter is equal to1000 cubic centimeters (1 l = 1000 cm ).3 2 in. x 3 in. x 5 in. = 30 in.3 Unit Systems FUNDAMENTAL DIMENSIONS Rev. 0 Page 7 CP-01 Density Density is a measure of themass of anobject per unitvolume;thus, it hasunits of mass divided by lengthcubed such as kilograms per cubic meter (kg/m ) or pounds3 per cubic foot (lbs/ft ).3 15 lbs/5 ft = 3 lbs/ft3 3 Velocity Velocity is the change in length per unit time;thus, it hasunits such as kilometers per hour (km/h) or feet per second (ft/s). Acceleration Acceleration is a measure of the change in velocity or velocity per unittime; thus, it has units such as centimeters per second per second (cm/s ) or feet per second per2 second (ft/s ).2 FUNDAMENTAL DIMENSIONS Unit Systems CP-01 Page 8 Rev. 0 Fundamental Dimensions Summary The fundamental measurements consist of: C Length - distance between two points C Mass - amount of material in an object C Time - duration between two instants The English system of units is based on the following standard units: C Foot C Pound C Second The SI system of measurement consists of the following standard units: MKS CGS C Meter C Centimeter C Kilogram C Gram C Second C Second Derived units are made up of a combination of units to describe various physical quantities. For example: C Area - square inches (in. )2 C Volume - cubic inches (in. ) or liters3 C Density - mass per volume (lb/in. )3 Summary The mainpoints of thischapter aresummarized below. Unit Systems UNIT CONVERSIONS Rev. 0 Page 9 CP-01 UNIT CONVERSIONS In order to apply measurements from the SI system to the English system, it is necessary to develop relationships ofknown equivalents (conversionfactors). These equivalents can then be used to convert from the given units of measure to the desired units of measure. EO 1.4 CONVERT between English and SI units of length. EO 1.5 CONVERT between English and SI units of mass. EO 1.6 CONVERT time measurements between the following: a. Years b. Weeks c. Days d. Hours e. Minutes f. Seconds Personnel at DOE nuclear facilties areoften exposed to both theEnglish and SI systems of units in their work. In some cases, the measurementsthat are taken or readfrom an instrumentwill be different from those required by a procedure.This situation will require the conversion of measurements to those required by theprocedure.

Conversion Factors Conversion factors are based on relationships of equivalentsfrom different measurement systems. These conversion factors are then applied to the givenmeasurement in order to convert it to the units that are required. The equivalent relationships between different units of measurement are defined in conversion tables. Someexamples from conversion tables are given below. C 1 yard = .9144 meters C 1 kilogram = 2.205poundsmass (lbm) C 1 hour = 3600 seconds 1 ft 1 ft ' 12 inches 1 foot or 1 ' 12 inches 1 foot 12 inches 1 foot UNIT CONVERSIONS Unit Systems CP-01 Page 10 Rev. 0 A typical conversion table is shown in Table 7. TABLE 7 Conversion Table Length 1 yd = 0.9144 m 12 in. = 1 ft 5280 ft = 1mile 1 m = 3.281 ft 1 in. = 0.0254 m Time 60 sec = 1 min 3600 sec = 1 hr Mass 1 lbm = 0.4535 kg 2.205 lbm = 1 kg 1 kg = 1000 g Area 1 ft = 144 in.2 2 10.764 ft = 1 m2 2 1 yd = 9 ft2 2 1 mile = 3.098 X 10 yd2 6 2 Volume 7.48 gal = 1 ft3 1 gal = 3.785 l (liter) 1 l = 1000 cm3 Unit Conversion To convertfrom one measurement unit toanother measurementunit (for example, toconvert 5 feet to inches), first select theappropriateequivalent relationship from the conversion table(for this example, 1 foot = 12 inches). Conversion isbasically a multiplication by 1. We can dividebothsides of the equation 1 ft = 12inches by 1foot to obtain the following. Then The relationship is a conversionfactorwhich we can use in our example toconvert 5 feet to inches. 1 ' 12 inches foot 5 feet ' 5 feet × 12 inches ft ' 5 × 12 inches' 60 inches. desired units present units 1 ' 3.281 ft 1 m (795 m) x 3.281 ft 1 m ' 795 m 1 x 3.281 ft 1 m Unit Systems UNIT CONVERSIONS Rev. 0 Page 11 CP-01 Using the example, 5feet is to be converted toinches. Startwith the obvious equation 5 ft = 5 ft, and multiply theright hand side by . 5 feet = 5 feet x 1 Thus, 5 feet is equivalent to 60 inches. Steps for Unit Conversion Using the following example, we will step through the process for converting from agiven set of units to a desired set of units. Convert 795 m to ft. Step 1. Select the equivalent relationship from the conversion table (Table 7). 1 meter = 3.281 ft Step 2. Divide toobtain the factor 1 as a ratio . Step 3. Multiply the quantity by the ratio. = 795 x 3.281 ft = 2608.395 ft 1' 3.098 x 106 sq yd 1 sq mile (2.91 sq miles) x 3.098 x 106 sq yd 1 sq mile ' 9.015 x 106 sq yd 1' 9 sq ft 1 sq yd (9.015 x 106 sq yd) x 9 sq ft 1 sq yd ' 8.114 x 107 sq ft 1' 1 sq m 10.764 sq ft UNIT CONVERSIONS Unit Systems CP-01 Page 12 Rev. 0 If an equivalent relationship between thegiven units and thedesired units cannot be found in the conversion tables, multipleconversion factors must be used. The conversion is performed inseveral steps until the measurement is in the desired units. The givenmeasurement must bemultiplied by each conversionfactor (ratio). After thecommon units have been canceledout, theanswerwill be in the desired units. Example: Convert 2.91 sqmiles to sqmeters. Step 1. Select the equivalent relationship from the conversion table. Becausethere is no direct conversion shown for squaremiles to square meters,multiple conversions will be necessary. For this example the following conversionswill be used. sq miles to sq yds to sq ft to sq m 1 sq mile = 3.098 x 10 sq yd6 1 sq yd = 9 sq ft 10.764 sq ft = 1 sq m Step 2. Express therelationship as aratio (desired unit/present unit). Step 3. Multiply the quantity by the ratio.

Step 4. Repeat the steps until the value is in thedesired units. (8.114 x 107 sq ft) x 1 sq m 10.764 sq ft ' (8.114 x 107) (1 sq m) 10.764 8.114 x 107 sq m 10.764 (2.91 sq miles) x 3.098 x 106 sq yd 1 sq mile x 9 sq ft 1 sq yd x 1 sq m 10.764 sq ft (2.91) x (3.098 x 106) (9) (1 sq m) 10.764 8.114 x 107 sq m 10.764 Unit Systems UNIT CONVERSIONS Rev. 0 Page 13 CP-01 = = 7.538 x 10 sq m6 It is possible toperform all of the conversions in asingleequation as long as all of theappropriate conversion factors areincluded. = = = 7.538 x 10 sq m6 Example: A Swedish firm isproducing avalvethat is to be used by anAmerican supplier. The Swedish firm uses the MKS system for allmachining. Toconform with the MKS system, howwill the following measurements be listed? Valve stem 57.20 in. Valve inlet andoutlet I.D. 22.00 in. O.D. 27.50 in. Solution: Valve stem 57.20 in. x 0.0254m/in. = 1.453 m Valve inlet andoutlet I.D. 22.00 x 0.0254 = 0.559 m O.D. 27.50 x 0.0254 = 0.699 m UNIT CONVERSIONS Unit Systems CP-01 Page 14 Rev. 0 TABLE 8 Conversion Factors CONVERSION FACTORS FOR COMMON UNITS OF MASS g kg t lbm 1 gram = 1 0.001 10 2.2046 x 10-6 -3 1 kilogram = 1000 1 0.001 2.2046 1 metric ton (t) = 10 1000 1 2204.66 1 pound-mass (lbm) = 453.59 0.45359 4.5359 x 10 1-4 1 slug = 14,594 14.594 0.014594 32.174 CONVERSION FACTORS FOR COMMON UNITS OF LENGTH cm m km in. ft mi 1 centimeter = 1 0.01 10 0.39370 0.032808 6.2137 X 10-5 -6 1 meter = 100 1 0.001 39.370 3.2808 6.2137 x 10-4 1 kilometer = 10 1000 1 39,370 3280.8 0.621375 1 inch = 2.5400 0.025400 2.5400 x 10 1 0.083333 1.5783 x 10-5 -5 1 foot = 30.480 0.30480 3.0480 x 10 12.000 1 1.8939 x 10-4 -4 1 mile = 1.6093 x 10 1609.3 1.6093 63,360 5280.0 15 Examples of common conversionfactors are shown in Table 8. Unit Systems UNIT CONVERSIONS Rev. 0 Page 15 CP-01 TABLE 8 (Cont.) Conversion Factors CONVERSION FACTORS FOR COMMON UNITS OF TIME sec min hr 1 second = 1 0.017 2.7 x 10-4 1 minute = 60 1 0.017 1 hour = 3600 60 1 1 day = 86,400 1440 24 1 year = 3.15 x 10 5.26 x 10 87607 5 day year 1 second = 1.16 x 10 3.1 x 10-5 -8 1 minute = 6.9 x 10 1.9 x 10-4 -6 1 hour = 4.16 x 10 1.14 x 10-2 -4 1 day = 1 2.74 x 10-3 1 year = 365 1 UNIT CONVERSIONS Unit Systems CP-01 Page 16 Rev. 0 Unit Conversion Summary C Conversion Tables list equivalent relationships. C Conversion Factors are obtained by dividing to get a multiplying factor (1). Unit Conversion Steps C Step 1 - Select the equivalent relationship from the conversion table. C Step 2 - Express the relationship as a conversion factor. C Step 3 - Multiply the given quantity by the conversion factor. Summary Unit conversion is summarized below. Department of Energy Fundamentals Handbook CLASSICAL PHYSICS Module 2 Vectors Vectors TABLE OF CONTENTS Rev. 0 Page i CP-02 TABLE OF CONTENTS LIST OF FIGURES. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . iii LIST OF TABLES. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . v REFERENCES. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . vi OBJECTIVES. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . vii

SCALAR AND VECTOR QUANTITIES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 Scalar Quantities. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 Vector Quantities. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 Description of a Simple Vector. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 Examples of Vector Quantities. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 Summary . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 VECTOR IDENTIFICATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 In Written Materials. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 Graphic Representation. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 Graphic Representation of Vectors. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5 Summary . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7 VECTORS: RESULTANTS AND COMPONENTS. . . . . . . . . . . . . . . . . . . . . . . . . . . 8 Resultant . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8 Vector Components. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10 Summary . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15 GRAPHIC METHOD OF VECTOR ADDITION. . . . . . . . . . . . . . . . . . . . . . . . . . . . 16 Vector Addition . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16 Methods Used to Add Vectors. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16 Using the Graphic Method. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16 Summary . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19 TABLE OF CONTENTS Vectors CP-02 Page ii Rev. 0 TABLE OF CONTENTS (Cont.) COMPONENT ADDITION METHOD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20 An Explanation of Components. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20 Using the Component Addition Method. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20 Summary. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 22 ANALYTICAL METHOD OF VECTOR ADDITION . . . . . . . . . . . . . . . . . . . . . . . . 23 Review of Mathematical Functions. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23 Using the Analytical Method. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 24 Summary. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 30 Vectors LIST OF FIGURES Rev. 0 Page iii CP-02 LIST OF FIGURES Figure 1 Vector Reference Axis. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 Figure 2 Vector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 Figure 3 Rectangular Coordinate System. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4

Figure 4 Displaying Vectors Graphically - Magnitude. . . . . . . . . . . . . . . . . . . . . . 5 Figure 5 Display Vectors Graphically - Direction. . . . . . . . . . . . . . . . . . . . . . . . . 6 Figure 6 Directional Coordinates. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6 Figure 7 Degree Coordinates. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7 Figure 8 Vector Addition in Same Direction. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8 Figure 9 Vector Addition in Opposite Direction. . . . . . . . . . . . . . . . . . . . . . . . . . 8 Figure 10 Vector Addition Not in Same Line. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9 Figure 11 Vector Components. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11 Figure 12 Component Vectors. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11 Figure 13 Right Triangle. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12 Figure 14 F = 50 lbf at 53E . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13R Figure 15 F = 80 lbf at 220E . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14R Figure 16 Rectangular Coordinate System. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16 Figure 17 Vector F . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 172 Figure 18 Resultant. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17 Figure 19 Graphic Addition - Example 1. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18 Figure 20 Graphic Addition - Example 2. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19 LIST OF FIGURES Vectors CP-02 Page iv Rev. 0 LIST OF FIGURES (Cont.) Figure 21 Vector Addition Component Method. . . . . . . . . . . . . . . . . . . . . . . . . . 20 Figure 22 Right Triangle. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23 Figure 23 Trigonometric Functions. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 24 Figure 24 Hypotenuse and Angle. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 24 Figure 25 Example Model 1. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 25 Figure 26 Example Model 2. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 26 Vectors LIST OF TABLES Rev. 0 Page v CP-02 LIST OF TABLES NONE REFERENCES Vectors CP-02 Page vi Rev. 0 REFERENCES C Beiser, Arthur, Applied Physics Schaums Outline Series, McGraw-Hill Book Company, 1976. C Murray, Raymond and Cobb, Grover, Physics Concepts and Consequences, Prentice-Hall, Inc., 1970. C Alexander, Joseph, et al., Physics for Engineering Technology, John Wiley and Sons, 1978. C Sears, Francis and Zemansky, Mark, University Physics, 3rd edition, Addison- Wesley Publishing Co. C Science and Fundamental Engineering (SAFE), Classical Physics, "Measure" Windsor, CT: Combustion Engineering, Inc., 1988. C Academic Program for Nuclear Power Plant Personnel, Volume II, General Physics Corporation, Library of Congress Card #A 397747, April 1982. Vectors OBJECTIVES Rev. 0 Page vii CP-02 TERMINAL OBJECTIVE 1.0 Using vectors, DETERMINE the net force acting on an object. ENABLING OBJECTIVES

1.1 DEFINE the following as they relate to vectors: a. Scalar quantity b. Vector quantity c. Vector component d. Resultant 1.2 DETERMINE components of a vector from a resultant vector. 1.3 ADD vectors using the following methods: a. Graphical b. Component addition c. Analytical Vectors CP-02 Page viii Rev. 0 Intentionally Left Blank Vectors SCALAR AND VECTOR QUANTITIES Rev. 0 Page 1 CP-02 Figure 1 Vector Reference Axis SCALAR AND VECTOR QUANTITIES Scalars are quantities that have magnitude only; they are independent of direction. Vectors have both magnitude and direction. The length of a vector represents magnitude. The arrow shows direction. EO 1.1 DEFINE the following as they relate to vectors: a. Scalar quantity b. Vector quantity Scalar Quantities Most of the physical quantities encountered in physics are either scalar or vector quantities. A scalar quantity is defined as a quantity that has magnitude only. Typical examples of scalar quantities are time, speed, temperature, and volume. A scalar quantity or parameter has no directional component, only magnitude. For example, the units for time (minutes, days, hours, etc.) represent an amount of time only and tell nothing of direction. Additional examples of scalar quantities are density, mass, and energy. Vector Quantities A vector quantity is defined as a quantity that has both magnitude and direction. To work with vector quantities, one must know the method for representing these quantities. Magnitude, or "size" of a vector, is also referred to as the vector's "displacement." It can be thought of as the scalar portion of the vector and is represented by the length of the vector. By definition, a vector has both magnitude and direction. Direction indicates how the vector is oriented relative to some reference axis, as shown in Figure 1. Using north/south and east/west reference axes, vector "A" is oriented in the NE quadrant with a direction of 45 north of theo EW axis. G iving direction to scalar "A" makes it a vector. The length of "A" is representative of its magnitude or displacement. SCALAR AND VECTOR QUANTITIES Vectors CP-02 Page 2 Rev. 0 Figure 2 Vector To help distinguish between a scalar and a vector, let's look at an example where the only information known is that a car is moving at 50 miles per hour. The information given (50 mph) only refers to the car's speed, which is a scalar quantity. It does not indicate the direction the car is moving. However, the same car traveling at 50 mph due east indicates the velocity of the car because it has magnitude (50 mph) and direction (due east); therefore, a vector is indicated. When a vector is diagrammed, a straight line is drawn to show the unit of length. An arrow is drawn on one end of the line. The length of the line represents the magnitude of the vector, and the arrow represents the direction of the vector. Description of a Simple Vector Vectors are simple straight lines used to illustrate the direction and magnitude of certain quantities. Vectors have a starting point at one end (tail) and an arrow at the opposite end (head), as shown in Figure 2. Examples of Vector Quantities Displacement, velocity, acceleration, and force are examples of vector quantities. Momentum and magnetic field strength are also good examples of vector quantities, although somewhat more difficult to understand. In each of these examples, the main ingredients of magnitude and direction are present.

Vectors SCALAR AND VECTOR QUANTITIES Rev. 0 Page 3 CP-02 Scalar and Vector Quantities Summary SCALAR QUANTITIES C Magnitude only C Independent of direction C Examples of scalars include: time, speed, volume, and temperature VECTOR QUANTITIES C Both magnitude and direction C Length represents magnitude C Arrow shows direction C Examples of vectors include: force, velocity, and acceleration Summary The important aspects of scalar and vector quantities are summarized below. VECTOR IDENTIFICATION Vectors CP-02 Page 4 Rev. 0 Figure 3 Rectangular Coordinate System VECTOR IDENTIFICATION Vectors are symbolized in specific ways in texts and on graphs, using letters or rectangular coordinates. In Written Materials In textbooks, vector quantities are often represented by simply using a boldfaced letter (A, B, C, R). Particular quantities are predefined (F - force, V - velocity, and A - acceleration). Vector quantities are sometimes represented by, , , . Regardless of the convention used, specific vector A B C R vv vv vv vv quantities must include magnitude and direction (for example, 50 mph due north, or 50 lbf at 90 ).o Graphic Representation Vector quantities are graphically represented using the rectangular coordinate system, a two-dimensional system that uses an x-axis and a y-axis. The x-axis is a horizonal straight line. The y-axis is a vertical straight line, perpendicular to the x-axis. An example of a rectangular system is shown in Figure 3. The intersection of the axes is called the point of origin. Each axis is marked off in equal divisions in all four directions from the point of origin. On the horizonal axis (x), values to the right of the origin are positive (+). Values to the left of the origin are negative (-). On the vertical axis (y), values above the point of origin are positive (+). Values below the origin are negative (-). It is very important to use the same units (divisions) on both axes. The rectangular coordinate system creates four infinite quadrants. Quadrant I is located above and to the right of the origin. Quadrant II is located above and to the left of the origin. Quadrant III is situated to the left and below the origin, and quadrant IV is located below and to the right of the origin (see Figure 3). Vectors VECTOR IDENTIFICATION Rev. 0 Page 5 CP-02 Figure 4 Displaying Vectors Graphically - Magnitude Graphic Representation of Vectors With the coordinate system defined, the following explanation will illustrate how to locate vectors in that system. First, using a ruler and graph paper, a rectangular coordinate system is laid out as described in the previous section. The x- and y-axes are labeled. Equal divisions are marked off in all four directions. Those to the right and above the point of origin are labeled positive (+). Those to the left and below the point of origin are labeled negative (-). Beginning at the point of origin (intersection of the axes), a line segment of the proper length is shown along the x-axis, in the positive direction. This line segment represents the vector magnitude, or displacement. An arrow is placed at the "head" of the vector to indicate direction. The "tail" of the vector is located at the point of origin (see Figure 4).

When vectors are drawn that do not fall on the x- or y-axes, the tail is located at the point of origin. Depending on the vector description, there are two methods of locating the head of the vector. If coordinates (x,y) are given, these values can be plotted to locate the vector head. If the vector is described in degrees, the line segment can be rotated counterclockwise from the x-axis to the proper orientation, as shown in Figure 5. VECTOR IDENTIFICATION Vectors CP-02 Page 6 Rev. 0 Figure 5 Display Vectors Graphically - Direction Figure 6 Directional Coordinates Because the x- and y-axes define direction, conventional directional coordinates and degrees may also be used to identify the x- and y-axes (see Figures 6 and 7). Vectors VECTOR IDENTIFICATION Rev. 0 Page 7 CP-02 Figure 7 Degree Coordinates Vector Identification Summary C In text: - Boldfaced letters ( A, F, R) - Capital letters with arrows over (, , )A F R vv vv vv C Graphically: - (x,y) coordinates - Directional Coordinates - Degrees Summary The main points covered in this chapter are summarized below. VECTORS: RESULTANTS AND COMPONENTS Vectors CP-02 Page 8 Rev. 0 Figure 8 Vector Addition in Same Direction Figure 9 Vector Addition in Opposite Directions VECTORS: RESULTANTS AND COMPONENTS A resultant is a single vector which represents the combined effect of two or more other vectors (called components). The components can be determined either graphically or by using trigonometry. EO 1.1 DEFINE the following as they relate to vectors: c. Vector component d. Resultant EO 1.2 DETERMINE components of a vector from a resultant vector. Resultant When two or more vectors are added they yield the sum or resultant vector. A resultant vector is the result or sum of vector addition. Vector addition is somewhat different from addition of pure numbers unless the addition takes place along a straight line. In the latter case, it reduces to the number line of standards or scale addition. For example, if one walks five miles east and then three miles east, he is eight miles from his starting point. On a graph (Figure 8), the sum of the two vectors, i.e., the sum of the five miles plus the three mile displacement, is the total or resultant displacement of eight miles. Similarly, if one walks five miles east and then three miles west, the resultant displacement is two miles east (Figure 9). The vector diagrams of Figure 8 and Figure 9 are basically scale diagrams of what is happening in the real world of addition of vector quantities. 5 inches × 1 mile inch ' 5 miles Vectors VECTORS: RESULTANTS AND COMPONENTS Rev. 0 Page 9 CP-02 Figure 10 Vector Addition Not in Same Line Consider next the addition of vector quantities which are not in a straight line. For example, consider the resultant displacement when a person travels four miles east and then three miles north. Again a scale drawing (Figure 10) is in order. Use a scale of 1 inch = 1 mile. When drawing a scale drawing, one draws a straight line from the origin C to the final position B to represent the net or resultant displacement. Drawing the straight line CB and measuring its length, one should obtain about 5 inches. Then, since the scale of the drawing is 1 inch = 1 mile, this is used as a conversion factor giving as the actual displacement. Using a protractor or trigonometry, the acute angle ACB can be determined to be about 37 .o

Thus, the resultant (or vector sum) of traveling 4 miles east plus 3 miles north is a displacement of 5 miles at 37 degrees north of east. VECTORS: RESULTANTS AND COMPONENTS Vectors CP-02 Page 10 Rev. 0 It is left as an exercise for the student to show that vector addition is commutative, using the above example. Specifically, make a scale drawing showing that traveling 3 miles north and then 4 miles east yields the same resultant as above. It is also reasonably obvious that more than two vectors can be added. One can travel three miles east and then three miles north and then three miles west and arrive at a point three miles north of the starting point. The sum of these three displacements is a resultant displacement of three miles north. (If this is not immediately apparent, sketch it.) A student problem is to find the net or resultant displacement if a person travels 9 miles south and then 12 miles east and then 25 miles north. Make a scale drawing and determine the magnitude and direction of the resultant displacement. A scale of 2 miles per centimeter or 4 miles per inch will fit the drawing on standard paper. Answer: About 20 miles at 53 north of east.o Vector Components Components of a vector are vectors, which when added, yield the vector. For example, as shown in the previous section (Figure 10), traveling 3 miles north and then 4 miles east yields a resultant displacement of 5 miles, 37 north of east. This example demonstrates thato component vectors of any two non-parallel directions can be obtained for any resultant vector in the same plane. For the purposes of this manual, we restrict our discussions to two dimensional space. The student should realize that vectors can and do exist in three dimensional space. One could write an alternate problem: "If I am 5 miles from where I started northeast along a line 37 N of east, how far north and how far east am I from my original position?" Drawing thiso on a scale drawing, the vector components in the east and north directions can be measured to be about 4 miles east and 3 miles north. These two vectors are the components of the resultant vector of 5 miles, 37 north of east.o Component vectors can be determined by plotting them on a rectangular coordinate system. For example, a resultant vector of 5 units at 53 can be broken down into its respective x and yo magnitudes. The x value of 3 and the y value of 4 can be determined using trigonometry or graphically. Their magnitudes and position can be expressed by one of several conventions including: (3,4), (x=3, y=4), (3 at 0 , 4 at 90 ), and (5 at 53 ). In the first expression, the firsto o o term is the x-component (F ), and the second term is the y-component (F ) of the associatedx y resultant vector. Vectors VECTORS: RESULTANTS AND COMPONENTS Rev. 0 Page 11 CP-02 Figure 11 Vector Components Figure 12 Component Vectors As in the previous example, if only the resultant is given, instead of component coordinates, one can determine the vector components as illustrated in Figure 11. First, plot t he resultant on rectangular coordinates and then project the vector coordinates to the axis. The length along the x-axis is F , and thex length along the y-axis is F . Thisy method is demonstrated in the following example. For the resultant vector shown in Figure 12, determine the component vectors given F = 50 lbf at 53 .R o First, project a perpendicular line from the head of F to the x-axis andR

a similar line to the y-axis. Where the projected lines meet, the axes determine the magnitude size of the component vectors. In this example, the component vectors are 30 lbf at 0 (F ) ando x 40 lbf at 90 (F ). If F had not already been drawn, the first step would have been to draw theo y R vector. sin2 ' opposite hypotenuse ' a c cos2 ' adjacent hypotenuse ' b c tan2 ' opposite adjacent ' a b VECTORS: RESULTANTS AND COMPONENTS Vectors CP-02 Page 12 Rev. 0 Figure 13 Right Triangle As an exercise, the student should graphically find the easterly and northerly components of a 13 mile displacement at 22.6 north of east. The correct answer is 5 miles east and 12 mileso north. Trigonometry may also be used to determine vector components. Before explaining this method, it may be helpful to review the fundamental trigonometric functions. Recall that trigonometry is a branch of mathematics that deals with the relationships between angles and the length of the sides of triangles. The relationship between an acute angle of a right triangle, shown in Figure 13, and its sides is given by three ratios. (2-1) (2-2) (2-3) Before attempting to calculate vector components, first make a rough sketch that shows the approximate location of the resultant vector in an x-y coordinate system. It is helpful to form a visual picture before selecting the correct trigonometric function to be used. Consider the example of Figure 12, that was used previously. This time the component vectors will be calculated. Vectors VECTORS: RESULTANTS AND COMPONENTS Rev. 0 Page 13 CP-02 Figure 14 F = 50 lbf at 53R o Example 1: Determine the component vectors, F and F , for F = 50 lbf at 53 in Figure 14.x y R o Use trigonometric functions. F is calculated as follows:x cos 2 = adjacent/hypotenuse cos 2 = F /F or F = F cos 2x R x R F = (50)(cos53 )x o F = (50)(0.6018)x F = 30 lbf on x-axisx F is calculated as follows:y sin 2 = opposite/hypotenuse sin 2 = F /F or F = F sin 2y R y R F = (F )(sin 2)y R F = (50)(sin 53 )y o F = (50)(0.7986)y F = 40 lbf on y-axisy Therefore, the components for F are F = 30 lbf at 0 and F = 40 lbf at 90 . Note that this resultR x y o o is identical to the result obtained using the graphic method. VECTORS: RESULTANTS AND COMPONENTS Vectors CP-02 Page 14 Rev. 0 Figure 15 F = 80 lbf at 220R o Example 2: What are the component vectors, given F = 80 lbf at 220 ? See Figure 15.R o F is calculated as follows:x cos 2 = adjacent/hypotenuse cos 2 = F /F or F = F cos 2x R x R F = (F )(cos 2)x R F = (80)(cos 220 )x o F = (80)(-0.766)x F = -61 lbf at 0 or 61 lbf at 180x o o Vectors VECTORS: RESULTANTS AND COMPONENTS Rev. 0 Page 15 CP-02 Vector Terminology Summary C A resultant is a single vector that can replace two or more vectors. C Components can be obtained for any two non-parallel directions if the vectors are in the same plane. Restricting the treatment to perpendicular directions and two dimensional space, the components of a vector are the two vectors in the x and y (or east- west and north-south) directions which produce the same effect as the original vector (or add to produce the original vector). C Components are determined from data, graphically or analytically. F is calculated as follows:y sin 2 = opposite/hypotenuse sin 2 = F /F or F = F sin 2y R y R F = F sin 2y R F = (80)(sin 220 )y o F = (80)(-0.6428)y

F = -51 lbf at 90 or 51 lbf at 270y o o Therefore, the components for F are F = 61 at 180 and F = 51 lbf at 270 .R x y o o Summary Vector terminology is summarized below. GRAPHIC METHOD OF VECTOR ADDITION Vectors CP-02 Page 16 Rev. 0 Figure 16 Rectangular Coordinate System GRAPHIC METHOD OF VECTOR ADDITION Vectors are added to determine the magnitude and direction of the resultant. EO 1.3 ADD vectors using the following methods: a. Graphical Vector Addition Component vectors are added to determine the resultant vector. For example, when two or more forces are acting on a single object, vector addition is used to determine the direction and magnitude of the net (resultant) force on the object. Consider an airplane that travels due east for 100 miles at 500 mph, then NE for 50 miles at 400 mph, and finally north for 500 miles at 500 mph. Vector addition can be used to determine the net distance the airplane is from its point of origin or to predict when it will arrive at its destination. Methods Used to Add Vectors Several methods have been developed to add vectors. In this chapter, the graphic method will be explained. The next chapter will explain the component addition method. Either one of these methods will provide fairly accurate results. If a high degree of accuracy is required, an analytical method using geometric and trigonometric functions is required. Using the Graphic Method Before attempting to use this method, the following equipment is needed: standard linear (nonlog) graph paper, ruler, protractor, and pencil. The graphic method utilizes a five-step process. Step 1. Plot the first vector on the rectangular (x-y) axes. a. Ensure that the same scale is used on both axes. b. Place the tail (beginning) of the first vector at the origin of the axes as shown in Figure 16. Vectors GRAPHIC METHOD OF VECTOR ADDITION Rev. 0 Page 17 CP-02 Figure 17 Vector F2 Figure 18 Resultant Step 2. Draw the second vector connected to the end of the first vector. a. Start the tail of the second vector at the head of the first vector. b. Ensure that the second vector is also drawn to scale. c. Ensure proper angular orientation of the second vector with respect to the axes of the graph (see Figure 17). Step 3. Add other vectors sequentially. a. Add one vector at a time. b. Always start the tail of the new vector at the head of the previous vector. c. Draw all vectors to scale and with proper angular orientation. Step 4. When all given vectors have been drawn, draw and label a resultant vector, F , from the point of originR of the axes to the head of the final vector. a. The tail of the resultant is the tail of the first vector drawn as shown in Figure 18. b. The head of the resultant is at the head of the last vector drawn. GRAPHIC METHOD OF VECTOR ADDITION Vectors CP-02 Page 18 Rev. 0 Figure 19 Graphic Addition - Example 1 Step 5. Determine the magnitude and direction of the resultant. a. Measure the displacement and angle directly from the graph using a ruler and a protractor. b. Determine the components of the resultant by projection onto the x- and y-axes. Example 1: What are the magnitude and direction of the resultant for the following: F = 31 units at 300 , F = 4 units at 60 , and F = 8 units at 180 ? The three vectors ando o o 2 3 their resultant are shown in Figure 19. Answer: F = 4 units at 150R o Example 2: Given X = 50 Ohms at 90 , R = 50 Ohms at 0 , and X = 50 Ohms at 270 , whatL c o o o

is the Resultant Z? (See Figure 20) Note: X is inductive reactance, X isL c capacitive reactance and Z is impedance. Answer: Z = 50 Ohms at 0o Vectors GRAPHIC METHOD OF VECTOR ADDITION Rev. 0 Page 19 CP-02 Figure 20 Graphic Addition - Example 2 Graphic Method Summary C Draw rectangular coordinates. C Draw first vector. C Draw second vector connected to the end (head) of first vector with proper angular orientation. C Draw remaining vectors, starting at the head of the preceding vector. C Draw resultant vector from the origin of axes to head of final vector. C Measure length of resultant. C Measure angle of resultant vector addition. Summary The steps of the graphic method of vector addition are summarized below. COMPONENT ADDITION METHOD Vectors CP-02 Page 20 Rev. 0 Figure 21 Vector Addition Component Method COMPONENT ADDITION METHOD Vector components are added along each axis to determine the magnitude and direction of the resultant. EO 1.3 ADD vectors using the following methods: b. Component addition An Explanation of Components The component addition method refers to the addition of vector coordinates on a rectangular (x,y) coordinate system. Coordinates, as seen in previous examples, locate a specific point in the system. Relative to vectors, that specific point is the head of the vector. There are two ways to locate that point. The head can be located by counting the units along the x-axis and the units along the y-axis, as illustrated in Figure 21, where the point has coordinates (4,3); i.e., the x component has a magnitude of 4 and the y component has a magnitude of 3. The head can also be found by locating a vector of the proper length on the positive side of the x-axis, with its tail at the intersection of the x- and y- axes. Then the vector is rotated a given number of degrees in the counterclockwise direction. In this example, the head of the vector is located five units at 36.9 . Five units is the length of the vector.o Using the Component Addition Method To add vectors using the component addition method, use the following four step method. Step 1. Determine x- and y-axes components of all original vectors. Step 2. Mathematically combine all x-axis components. Note: When combining, recognize that positive x components at 180 are equivalento to negative x components at 0 (+x at 180 = -x at 0 ).o o o Vectors COMPONENT ADDITION METHOD Rev. 0 Page 21 CP-02 3. Mathematically combine all y-axis components (+y at 270 = -y at 90 ).o o 4. Resulting (x,y) components are the (x,y) components of the resulting vector. The following examples illustrate vector addition using the component addition method. Example 1: Given the following vectors what are the coordinates of the resultant vector, that is, the sum of the vectors? F = (4,10), F = (-6,4), F = (2,-4), and F = (10,-2)1 2 3 4 Step 1. Determine the x- and y-axes components of all four original vectors. x-axes components = 4, -6, 2, 10 y-axes components = 10, 4, -4, -2 Step 2. Mathematically combine all x-axis components. F = 4 + (-6) + 2 + 10x F = 4 - 6 + 2 + 10x F = 10x Step 3. Mathematically combine all y-axis components. F = 10 + 4 + (-4) + (-2)y F = 10 + 4 - 4 - 2y F = 8y Step 4. Express the resultant vector. The resultant components from the previous additions are the coordinates of the resultant, that is, F = (10,8).R Example 2: Determine the resultant, F .R Given: F = 30 lbf at 0 , 10 lbf at 901 o o

F = 50 lbf at 0 , 50 lbf at 902 o o F = 45 lbf at 180 , 30 lbf at 903 o o F = 15 lbf at 0 , 50 lbf at 2704 o o COMPONENT ADDITION METHOD Vectors CP-02 Page 22 Rev. 0 Component Addition Method Summary C Determine the x- and y- axes of all original vectors. C Mathematically combine all x-axis components. C Mathematically combine all y-axis components. C The results are the components of the resultant vector. Follow the sequence used in the first example. Remember that x at 180 is -x at 0 , and y ato o 270 is -y at 90 .o o F = 30 + 50 +(-45) + 15 = 50 lbfx F = 10 + 50 + 30 + (-50) = 40 lbfy F = 50 lbf at 0 , 40 lbf at 90R o o Summary The sequence of steps used in the component addition method of adding vectors is summarized below. c2 ' a2 % b2 or c ' a2 % b2 Vectors ANALYTICAL METHOD OF VECTOR ADDITION Rev. 0 Page 23 CP-02 Figure 22 Right Triangle ANALYTICAL METHOD OF VECTOR ADDITION Vector components are added to determine the magnitude and direction of the resultant. Calculations using trigonometric functions are the most accurate method for making this determination. EO 1.3 ADD vectors using the following methods: c. Analytical The graphic and components addition methods of obtaining the resultant of several vectors described in the previous chapters can be hard to use and time consuming. In addition, accuracy is a function of the scale used in making the diagram and how carefully the vectors are drawn. The analytical method can be simpler and far more accurate than these previous methods. Review of Mathematical Functions In earlier mathematics lessons, the Pythagorean Theorem was used to relate the lengths of the sides of right triangles such as in Figure 22. The Pythagorean Theorem states that in any right triangle, the square of the length of the hypotenuse equals the sum of the squares of the lengths of the other two sides. This expression may be written as given in Equation 2-4. (2-4) ANALYTICAL METHOD OF VECTOR ADDITION Vectors CP-02 Page 24 Rev. 0 Figure 23 Trigonometric Functions Figure 24 Hypotenuse and Angle Also, recall the three trigonometric functions reviewed in an earlier chapter and shown in Figure 23. The cosine will be used to solve for F . The sine will be used to solve for F .x y Tangent will normally be used to solve for 2, although sine and cosine may also be used. On a rectangular coordinate system, the sine values of 2 are positive (+) in quadrants I and II and negative (-) in quadrants III and IV. The cosine values of 2 are positive (+) in quadrants I and IV and negative (-) in quadrants II and III. Tangent values are positive (+) in quadrants I and III and negative (-) in quadrants II and IV. When mathematically solving for tan 2, calculators will specify angles in quadrants I and IV only. Actual angles may be in quadrants II and III. Each problem should be analyzed graphically to report a realistic solution. Quadrant II and III angles may be obtained by adding or subtracting 180 from the value calculated.o Using the Analytical Method To illustrate this method, consider this example: a man walks 3 miles in one direction, then turns 90 and continues to walk for an additional 4 miles. In what direction and how far is he from hiso starting point? The first step in solving this problem is to draw a simple sketch as shown in Figure 24. R ' a2 % b2 R ' 32 % 42 R ' 25 R ' 5 miles Vectors ANALYTICAL METHOD OF VECTOR ADDITION Rev. 0 Page 25 CP-02

Figure 25 Example Model 1 His net displacement is found using equation 2-4. His direction (angle of displacement) is found using the tangent function. tan 2 = opposite/adjacent tan 2 = a/b tan 2 = 4/3 tan 2 = 1.33 2 = tan 1.33-1 2 = 53o Therefore, his new location is 5 miles at 53 from his starting point.o By carrying this approach a step further, a model has been developed for finding the resultant of several vectors. For the purpose of developing the model, consider three forces (F , F , and F )1 2 3 acting on an object as shown in Figure 25. The goal is to find the resultant force (F ).R ANALYTICAL METHOD OF VECTOR ADDITION Vectors CP-02 Page 26 Rev. 0 Figure 26 Example Model 2 Step 1: Draw x and y coordinates and the three forces from the point of origin or the center of the object, as shown in Figure 26. Component vectors and angles have been added to the drawing to aid in the discussion. FR ' F2 Rx % F2 Ry tan2 ' FRy FRx 2 ' tan&1 FRy FRx Vectors ANALYTICAL METHOD OF VECTOR ADDITION Rev. 0 Page 27 CP-02 Step 2: Resolve each vector into its rectangular components. Vector Angle x component y component F 2 F = F cos2 F = F sin21 F 2 F = F cos2 F = F sin22 F 2 F = F cos2 F = F sin23 1 2 3 1x 1 1 2x 2 2 3x 3 3 1y 1 1 2y 2 2 3y 3 3 Step 3: Sum the x and y components. F = EF = F + F + FRx x 1x 2x 3x F = EF = F + F + FRy y 1y 2y 3y Where "E" means summation Step 4: Calculate the magnitude of F .R Step 5: Calculate the angle of displacement. ANALYTICAL METHOD OF VECTOR ADDITION Vectors CP-02 Page 28 Rev. 0 Force Magnitude Angle x component y component F 90 lbf 39 F = 90 cos 39 F = 90 sin 391 1x 1y o o o F = (90) (.777) F = (90) (.629)1x 1y F = 69.9 lbf F = 56.6 lbf1x 1y F 50 lbf 120 F = 50 cos 120 F = 50 sin 1202 2x 2y o o o F = (50) (-.5) F = (50) (.866)2x 2y F = -25 lbf F = 43.3 lbf2x 2y F 125 lbf 250 F = 125 cos 250 F = 125 sin 2503 3x 3y o o o F = (125) (-.342) F = (125) (-.94)3x 3y F = -42.8 lbf F = -117.5 lbf3x 3y Here is an example using this model. Follow it through step by step. Example: Given three forces acting on an object, determine the magnitude and direction of the resultant force F .R F = 90 lbf at 391 o F = 50 lbf at 1202 o F = 125 lbf at 2503 o Step 1: First draw x and y coordinate axes on a sheet of paper. Then, draw F , F ,1 2 and F from the point of origin. It is not necessary to be totally accurate3 in placing the vectors in the drawing. The approximate location in the right quadrant is all that is necessary. Label the drawing as in the model (Figure 26). Step 2: Resolve each force into its rectangular coordinates. F2 x % F2 y (2.1)2 % (&17.6)2 314.2 Vectors ANALYTICAL METHOD OF VECTOR ADDITION Rev. 0 Page 29 CP-02 Step 3: Sum the x and y components. F = F + F + FRx 1x 2x 3x F = 69.9 lbf + (-25 lbf) + (-42.8 lbf)Rx F = 2.1 lbfRx F = F + F + FRy 1y 2y 3y F = 56.6 lbf + 43.3 lbf + (-117.5 lbf)Ry F = -17.6 lbfRy Step 4: Calculate the magnitude of F .R F = R F = R F = R F = 17.7 lbfR Step 5: Calculate the angle of displacement. tan 2 = F /FRy Rx tan 2 = -17.6/2.1 tan 2 = -8.381 2 = tan (-8.381)-1 2 = -83.2o Therefore, F = 17.7 lbf at -83.2 or 276.8 .R o o Note: A negative angle means a clockwise rotation from the zero axis. It is left to the student to try the previous example using the other methods of vector addition described in earlier chapters.

ANALYTICAL METHOD OF VECTOR ADDITION Vectors CP-02 Page 30 Rev. 0 Analytical Method of Adding Vectors Summary C Draw x and y coordinate axes. C Draw component vectors from point of origin. C Resolve each vector into rectangular components. C Sum x and y components. C Calculate magnitude of F .R C Calculate angle of displacement. Summary The steps followed when using the analytical method to find the resultant of several vectors are summarized below. Department of Energy Fundamentals Handbook CLASSICAL PHYSICS Module 3 Force and Motion Force and Motion TABLE OF CONTENTS Rev. 0 Page i CP-03 TABLE OF CONTENTS LIST OF FIGURES. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ii LIST OF TABLES. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . iii REFERENCES. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . iv OBJECTIVES. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . v NEWTON'S LAWS OF MOTION. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 Summary. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 MOMENTUM PRINCIPLES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5 Momentum . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5 Force and Momentum. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6 Conservation of Momentum. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7 Summary. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10 LIST OF FIGURES Force and Motion CP-03 Page ii Rev. 0 LIST OF FIGURES Figure 1 Momentum . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8 Force and Motion LIST OF TABLES Rev. 0 Page iii CP-03 LIST OF TABLES NONE REFERENCE Force and Motion CP-03 Page iv Rev. 0 REFERENCES C Beiser, Arthur, Applied Physics Schaums Outline Series, McGraw-Hill Book Company, 1976. C Murray, Raymond and Cobb, Grover, Physics Concepts and Consequences, Prentice-Hall, Inc., 1970. C Alexander, Joseph, et al., Physics for Engineering Technology, John Wiley and Sons, 1978. C Sears, Francis and Zemansky, Mark, University Physics, 3rd edition, Addison- Wesley Publishing Co. C Science and Fundamental Engineering (SAFE), Classical Physics, "Measure" Windsor, CT: Combustion Engineering, Inc., 1988. C Academic Program for Nuclear Power Plant Personnel, Volume II, General Physics Corporation, Library of Congress Card #A 397747, April 1982. Force and Motion OBJECTIVES Rev. 0 Page v CP-03 TERMINAL OBJECTIVE 1.0 APPLY Newton's laws of motion to a body. ENABLING OBJECTIVES 1.1 STATE Newton's first law of motion. 1.2 STATE Newton's second law of motion. 1.3 STATE Newton's third law of motion. 1.4 STATE Newton's law of universal gravitation. 1.5 DEFINE momentum. 1.6 EXPLAIN the conservation of momentum. 1.7 Using the conservation of momentum, CALCULATE the velocity for an object (or objects) following a collision of two objects.

Force and Motion CP-03 Page vi Rev. 0 Intentionally Left Blank F ' ma Force and Motion NEWTON'S LAWS OF MOTION Rev. 0 Page 1 CP-03 NEWTON'S LAWS OF MOTION The study of Newton's laws of motion allows us to understand and accurately describe the motion of objects and the forces that act on those objects. EO 1.1 STATE Newton's first law of motion. EO 1.2 STATE Newton's second law of motion. EO 1.3 STATE Newton's third law of motion. EO 1.4 STATE Newton's law of universal gravitation. The basis for modern mechanics was developed in the seventeenth century by Sir Isaac Newton. From his studies of objects in motion, he formulated three fundamental laws. Newton's first law of motion states "an object remains at rest (if originally at rest) or moves in a straight line with constant velocity if the net force on it is zero." Newton's second law states "the acceleration of a body is proportional to the net (i.e., sum or resultant) force acting on it and in the direction of that net force." This law establishes the relationship between force, mass, and acceleration and can be written mathematically as shown in Equation 3-1. (3-1) where: F = force (Newton = 1 Kg-m/sec , or lbf)2 m = mass (Kg or lbm) a = acceleration (m/sec or ft/sec )2 2 This law is used to define force units and is one of the most important laws in physics. Also, Newton's first law is actually a consequence of this second law, since there is no acceleration when the force is zero, and the object is either at rest or moving with a constant velocity. Equation 3-1 can be used to calculate an objects weight at the surface of the earth. In this special case, F is the force, or weight, caused by the gravitational acceleration of the earth acting on the mass, m, of the object. When dealing with this type of problem, we designate the acceleration, g, which equals 9.8m/sec or 32.17 ft/sec (g is called gravitational acceleration constant). Thus, equation 3-12 2 becomes F = mg for this case. F ' G m1m2 r 2 lbm & ft 2 slug2 NEWTON'S LAWS OF MOTION Force and Motion CP-03 Page 2 Rev. 0 Newton's third law of motion states "if a body exerts a force on a second body, the second body exerts an equal and opposite force on the first." This law has also been stated as, "for every action there is an equal and opposite reaction." The third law is basic to the understanding of force. It states that forces always occur in pairs of equal and opposite forces. Thus, the downward force exerted on a desk by a pencil is accompanied by an upward force of equal magnitude exerted on the pencil by the desk. This principle holds for all forces, variable or constant, regardless of their source. One additional law attributed to Newton concerns mutual attractive forces between two bodies. It is known as the universal law of gravitation and is stated as follows. "Each and every mass in the universe exerts a mutual, attractive gravitational force on every other mass in the universe. For any two masses, the force is directly proportional to the product of the two masses and is inversely proportional to the square of the distance between them." Newton expressed the universal law of gravitation using Equation 3-2. (3-2) where: F = force of attraction (Newton = 1Kg-m/sec or lbf)2 G = universal constant of gravitation (6.673 x 10 m /kg-sec or 3.44 x 10-11 3 2 -8 ) m = mass of the first object (Kg or lbm)1 m = mass of the second object (Kg or lbm)2

r = distance between the centers of the two objects (m or ft) Using this universal law of gravitation, we can determine the value of g (gravitational acceleration constant), at the surface of the earth. We already know this value to be 9.8 m/sec (or 32.172 ft/sec ), but it can be calculated using Equation 3-2.2 Calculation: First, we will assume that the earth is much larger than the object and that the object resides on the surface of the earth; therefore, the value of r will be equal to the radius of the earth. Second, we must understand that the force of attraction (F) in Equation 3-2 for the object is equal to the object's weight (F) as described in Equation 3.1. Setting these two equations equal to each other yields the following. F ' G Mem1 r 2 ' m1a g ' G Me r 2 g ' 6.673×10&11 m3 kg sec2 5.95×1024 kg (6.367×106 m)2 g ' 9.8 m sec2 r ' 30000 m% 6.367×106 m ' 6.397×106 m g ' 6.673×10&11 m3 kg sec2 5.95×1024 kg (6.397×106 m)2 g ' 9.7 m sec2 Force and Motion NEWTON'S LAWS OF MOTION Rev. 0 Page 3 CP-03 where: M = mass of the earth (5.95 x 10 kg)e 24 m = mass of the object1 r = radius of the earth (6.367 x 10 m)6 The mass (m ) of the object cancels, and the value of (g) can be determined as follows1 since a=g by substituting (g) for (a) in the previous equation. If the object is a significant distance from the earth, we can demonstrate that (g) is not a constant value but varies with the distance (altitude) from the earth. If the object is at an altitude of 30 km (18.63 mi), then the value of (g) is as follows: As you can see, a height of 30 km only changes (g) from 9.8 m/sec to 9.7 m/sec . There2 2 will be an even smaller change for objects closer to the earth. Therefore, (g) is normally considered a constant value since most calculations involve objects close to the surface of the earth. NEWTON'S LAWS OF MOTION Force and Motion CP-03 Page 4 Rev. 0 Newton's Laws of Motion Summary Newton's First Law of Motion An object remains at rest (if originally at rest) or moves in a straight line with constant velocity if the net force on it is zero. Newton's Second Law of Motion A particle with a force acting on it has an acceleration proportional to the magnitude of the force and in the direction of that force. Newton's Third Law of Motion The forces of action and reaction between interacting bodies are equal in magnitude and opposite in direction. - or - For every action there is an equal and opposite reaction. Newton's Universal Law of Gravitation Each and every mass in the universe exerts a mutual, attractive gravitational force on every other mass in the universe. For any two masses, the force is directly proportional to the product of the two masses and is inversely proportional to the square of the distance between them. Summary Newton's laws of motion are summarized below. Force and Motion MOMENTUM PRINCIPLES Rev. 0 Page 5 CP-03 MOMENTUM PRINCIPLES Momentum is a measure of the motion of a moving body. An understanding of momentum and the conservation of momentum provides essential tools in solving physics problems. EO 1.5 DEFINE momentum. EO 1.6 EXPLAIN the conservation of momentum. EO 1.7 Using the conservation of momentum, CALCULATE the velocity for an object (or objects) following a collision of two objects. Momentum Momentum is a basic and widely applicable concept of physics. It is, in a sense, the measure of the motion of a moving body. It is the result of the product of the body's mass and the velocity at which it is moving. Therefore, momentum can be defined using Equation 3-3.

P = mv (3-3) where: P = momentum of the object (Kg-m/sec or ft-lbm/sec) m = mass of the object (Kg or lbm) v = velocity of the object (m/sec or ft/sec) Momentum is a vector quantity since it results from the velocity of the object. If different momentum quantities are to be added vectorially, the direction of each momentum must be taken into account. However, to simplify the understanding of momentum, only straight line motions will be considered. Example: Calculate the momentum for a 16 lbm bowling ball rolling down a lane at 22 ft/sec. P ' mv P ' (16 lbm) 22 ft sec P ' 352 ft&lbm sec F ' ma a ' (v & vo) (t & to) F ' m v & vo t & to F ' mv & mvo t & to F ' P & Po t & to F ' )P )t MOMENTUM PRINCIPLES Force and Motion CP-03 Page 6 Rev. 0 Solution: Force and Momentum There is a direct relationship between force and momentum. The rate at which momentum changes with time is equal to the net force applied to an object. This relationship comes directly from Newton's second law of motion, F = ma. This is a special case of Newton's second law for a constant force which gives rise to a constant acceleration. The linking fact is that acceleration is the rate at which velocity changes with time. Therefore, we can determine the following: We know that, and since, then, (3-4) which can also be written, (3-5) Substituting P for mv and P for mv , o o or (3-6) From Equation 3-6, we can determine that force (F) is equal to the change in momentum per time. F ' m v & vo t & to F ' 10000 lbm 110 ft/sec 9 sec F ' 1.2×105 ft&lbm sec2 mGvG % mBvB ' 0 or mGvG ' &mBvB Force and Motion MOMENTUM PRINCIPLES Rev. 0 Page 7 CP-03 Example: The velocity of a rocket must be increased by 110 ft/sec to achieve proper orbit around the earth. If the rocket has a mass of 5 tons and it takes 9 sec. to reach orbit, calculate the required thrust (force) to achieve this orbit. Solution: Even though the initial velocity (v ) and final velocity (v) are unknown, we do know theo change in velocity (v-v ), which is 110 ft/sec. Therefore, using Equation 3-4 we can findo the solution. Conservation of Momentum One of the most useful properties of momentum is that it is conserved. This means that if no net external force acts upon an object, the momentum of the object remains constant. Using Equation 3-6, we can see that if force (F) is equal to zero, then )P = 0. It is most important for collisions, explosions, etc., where the external force is negligible, and states that the momentum before the event (collision, explosion) equals the momentum following the event. The conservation of momentum applies when a bullet is fired from a gun. Prior to firing the gun, both the gun and the bullet are at rest (i.e., V and V are zero), and therefore the totalG B momentum is zero. This can be written as follows: When the gun is fired, the momentum of the recoiling gun is equal and opposite to the momentum of the bullet. That is, the momentum of the bullet (m v ) is equal to the momentumB B of the gun (m v ), but of opposite direction.G G j Pinitial ' j Pfinal MOMENTUM PRINCIPLES Force and Motion CP-03 Page 8 Rev. 0 Figure 1 Momentum

The development of the law of conservation of momentum does not consider whether the collision is elastic or inelastic. In an elastic collision, both momentum and kinetic energy (i.e., energy due to an objects velocity) are conserved. A common example of an elastic collision is the head-on collision of two billiard balls of equal mass. In an inelastic collision, momentum is conserved, but system kinetic energy is not conserved. An example of an inelastic collission is the head-on collision of two automobiles where part of the initial kinetic energy is lost as the metal crumples during the impact. The concept of kinetic energy will be discussed further in Module 5 of this course. The law of conservation of momentum can be mathematically expressed in several different ways. In general, it can be stated that the sum of a system's initial momentum is equal to the sum of a system's final momentum. (3-7) In the case where a collision of two objects occurs, the conservation of momentum can be stated as follows. P + P = P + P (3-8)1 initial 2 initial 1 final 2 final or (m v ) + (m v ) = (m v ) + (m v ) (3-9)1 1 initial 2 2 initial 1 1 final 2 2 final In the case where two bodies collide and have identical final velocities, equation 3-10 applies. m v + m v = (m + m )v (3-10)1 1 2 2 1 2 f For example, consider two railroad cars rolling on a level, frictionless track (see Figure 1). The cars collide, become coupled, and roll together at a final velocity (v ). The momentum beforef and after the collision is expressed with Equation 3-10. vf ' m1v1 % m2v2 m1 % m2 vf ' m1v1 % m2v2 m1 % m2 vf ' (2300 lbm)(29 ft/sec)% (2800 lbm)(11 ft/sec) 2300lbm% 2800 lbm vf ' 19.1 ft/sec Force and Motion MOMENTUM PRINCIPLES Rev. 0 Page 9 CP-03 If the initial velocities of the two objects (v and v ) are known, then the final velocity (v ) can1 2 f be calculated by rearranging Equation 3-10 into Equation 3-11. (3-11) Example: Consider that the railroad cars in Figure 1 have masses of m = 2300 lbm and1 m = 2800 lbm. The first car (m ) is moving at a velocity of 29 ft/sec and the second car2 1 (m ) is moving at a velocity of 11 ft/sec. The first car overtakes the second car and2 couples with it. Calculate the final velocity of the two cars. Solution: The final velocity (v ) can be easily calculated using Equation 3-8.f MOMENTUM PRINCIPLES Force and Motion CP-03 Page 10 Rev. 0 Summary The concepts of momentum and the conservation of momentum are summarized below. Momentum Summary Momentum is the measure of the motion of a moving body. It is the result of the product of the body's mass and the velocity at which it is moving. Therefore, momentum can be defined as: P = mv. The conservation of momentum states that if no net external force acts upon a system, the momentum of the system remains constant. If force (F) is equal to zero, then )P = 0. The momentum before and after a collision can be calculated using the following equation. (m v ) + (m v ) = (m v ) + (m v )1 1 initial 2 2 initial 1 1 final 2 2 final Department of Energy Fundamentals Handbook CLASSICAL PHYSICS Module 4 Application of Newton's Laws Application of Newton's Laws TABLE OF CONTENTS Rev. 0 Page i CP-04 TABLE OF CONTENTS LIST OF FIGURES. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ii LIST OF TABLES. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . iii

REFERENCES. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . iv OBJECTIVES. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . v FORCE AND WEIGHT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 Force . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 Weight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 Summary . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 FREE-BODY DIAGRAMS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5 Constructing a Free-Body Diagram. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6 Summary . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10 FORCE EQUILIBRIUM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11 Net Force. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11 Equilibrium . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12 Summary . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16 TYPES OF FORCE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17 Tensile and Compressive Forces. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17 Friction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 17 Centripetal Force. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19 Centrifugal Force. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20 Summary . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21 LIST OF FIGURES Application of Newton's Laws CP-04 Page ii Rev. 0 LIST OF FIGURES Figure 1 Book on a Table. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6 Figure 2 Car . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7 Figure 3 Free-Body Diagram. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8 Figure 4 Various Free-Body Diagrams. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9 Figure 5 Net Force. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12 Figure 6 Hanging Object. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13 Figure 7 Free-Body Diagram. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14 Figure 8 Free-Body Diagram. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15 Figure 9 Frictional Forces. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18

Figure 10 Centripetal Force. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19 Figure 11 Centrifugal Force. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20 Figure 12 Loss of Centripetal Force. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20 Application of Newton's Laws LIST OF TABLES Rev. 0 Page iii CP-04 LIST OF TABLES NONE REFERENCES Application of Newton's Laws CP-04 Page iv Rev. 0 REFERENCES C Beiser, Arthur, Applied Physics Schaums Outline Series, McGraw-Hill Book Company, 1976. C Murray, Raymond and Cobb, Grover, Physics Concepts and Consequences, Prentice-Hall, Inc., 1970. C Alexander, Joseph, et al., Physics for Engineering Technology, John Wiley and Sons, 1978. C Sears, Francis and Zemansky, Mark, University Physics, 3rd edition, Addison- Wesley Publishing Co. C Science and Fundamental Engineering (SAFE), Classical Physics, "Measure" Windsor, CT: Combustion Engineering, Inc., 1988. C Academic Program for Nuclear Power Plant Personnel, Volume II, General Physics Corporation, Library of Congress Card #A 397747, April 1982. Application of Newton's Laws OBJECTIVES Rev. 0 Page v CP-04 TERMINAL OBJECTIVE 1.0 From memory, APPLY the principles of force to stationary or moving bodies. ENABLING OBJECTIVES 1.1 DEFINE the following: a. Force b. Weight 1.2 STATE the purpose of a free-body diagram. 1.3 Given all necessary information, CONSTRUCT a free-body diagram. 1.4 STATE the conditions necessary for a body to be in force equilibrium. 1.5 DEFINE the following: a. Net force b. Equilibrant 1.6 DEFINE the following: a. Tensile force b. Compressive force c. Frictional force 1.7 EXPLAIN the difference between a static-friction force and a kinetic-friction force. 1.8 STATE two factors that affect the magnitude of the friction force. 1.9 EXPLAIN the difference between centripetal force and centrifugal force. Application of Newton's Laws CP-04 Page vi Rev. 0 Intentionally Left Blank Application of Newton's Laws FORCE AND WEIGHT Rev. 0 Page 1 CP-04 FORCE AND WEIGHT Force can be thought of simply as a push or pull, but is more clearly defined as any action on a body that tends to change the velocity of the body. Weight is a force exerted on an object due to the object's position in a gravitational field. EO 1.1 DEFINE the following: a. Force b. Weight Introduction In the study of forces, the student must make valid assumptions called for in the formulation of real problems. The ability to understand and make use of the correct assumptions in the formulation and solution of engineering problems is certainly one of the most important abilities of a successful operator. One of the objectives of this manual is to provide an opportunity to develop this ability through the study of the fundamentals and the analysis of practical problems. An effective method of attack on all engineering problems is essential. The development of good habits in formulating problems and in representing their solutions will prove to be a valuable asset. Each solution should proceed with a logical sequence of steps from hypothesis to conclusion, and its representation should include a clear statement of the following parts, each clearly defined: a) given data, b) results desired, c) necessary diagrams, d) calculations, and e) answers and conclusions. Many problems become clear and straightforward once they are begun with a logical and disciplined method of attack.

In addition, it is important to incorporate a series of checks on the calculations at intermediate points in the solution. Also, all work must be neat and orderly. The subject of classical physics is based on surprisingly few fundamental concepts and involves mainly the application of these basic relations to a variety of situations. Newton's laws of motion are some of the fundamental concepts used in the study of force and weight. F ' ma W ' mg gc FORCE AND WEIGHT Application of Newton's Laws CP-04 Page 2 Rev. 0 Force Force is defined as a vector quantity that tends to produce an acceleration of a body in the direction of its application. Changing the body's velocity causes the body to accelerate. Therefore, force can be mathematically defined as given by Newton's second law of motion (Equation 4-1). (4-1) where: F = force on object (Newton or lbf) m = mass of object (Kg or lbm) a = acceleration of object (m/sec or ft/sec )2 2 Force is characterized by its point of application, its magnitude, and its direction. A force that is actually distributed over a small area of the body upon which it acts may be considered a concentrated force if the dimensions of the area involved are small compared with other pertinent dimensions. Two or more forces may act upon an object without affecting its state of motion. For example, a book resting upon a table has a downward force acting on it caused by gravity and an upward force exerted on it from the table top. These two forces cancel and the net force of the book is zero. This fact can be verified by observing that no change in the state of motion has occurred. Weight Weight is a special application of the concept of force. It is defined as the force exerted on an object by the gravitational field of the earth, or more specifically the pull of the earth on the body. (4-2) where: W = weight (lbf) m = mass (lbm) of the object g = the local acceleration of gravity (32.17 ft/sec )2 g = a conversion constant employed to facilitate the use of Newton's second law ofc motion with the English system of units and is equal to 32.17 ft-lbm/lbf-sec2 Note that g has the same numerical value as the acceleration of gravity at sea level.c W ' mg gc ' (185 lbm) 32.17 ft sec2 32.17 ft&lbm lbf&sec2 ' 185 lbf W ' mg gc ' (185 lbm) 5.36 ft sec2 32.17 ft&lbm lbf&sec2 ' 28.19 lbf Application of Newton's Laws FORCE AND WEIGHT Rev. 0 Page 3 CP-04 The mass of a body is the same wherever the body is, whether on the moon or on the earth. The weight of a body, however, depends upon the local acceleration of gravity. Thus, the weight of an object is less on the moon than on the earth because the local acceleration of gravity is less on the moon than on the earth. Example: Calculate the weight of a person with a mass of 185 lbm. Example: Calculate the weight of a person with a mass of 185 lbm on the moon. Gravity on the moon is 5.36 ft/sec .2 FORCE AND WEIGHT Application of Newton's Laws CP-04 Page 4 Rev. 0 Force and Weight Summary C Force is a vector quantity that tends to produce an acceleration of a body in the direction of its application. or F = ma C Weight is the force exerted on an object due to gravity. (On the earth it is the gravitational pull of the earth on the body.) W = mg/gc

With the idea of mass and weight understood, especially their differences, the concept of gravitational force is more easily explained. Any object that is dropped will accelerate as it falls, even though it is not in physical contact with any other body. To explain this, the idea of gravitational force was developed, resulting in the concept that one body, such as the earth, exerts a force on another body, even though they are far apart. The gravitational attraction of two objects depends upon the mass of each and the distance between them. This concept is known as Newton's law of gravitation, which was introduced in an earlier chapter. Summary The important concepts of force and weight are summarized below. Application of Newton's Laws FREE-BODY DIAGRAMS Rev. 0 Page 5 CP-04 FREE-BODY DIAGRAMS In studying the effect of forces on a body it is necessary to isolate the body and determine all forces acting upon it. This method of using a free-body diagram is essential in understanding basic and complex force problems. EO 1.2 STATE the purpose of a free-body diagram. EO 1.3 Given all necessary information, CONSTRUCT a free-body diagram. In solving a problem involving forces it is essential that Newton's laws are carefully fixed in mind and that these principles are applied literally and exactly. In applying these principles it is essential that the body be isolated from all other bodies so that a complete and accurate account of all forces which act on this body may be considered. The diagram of such an isolated body with the representation of all external forces acting on it is called a Free-Body Diagram. It has long been established that the free-body-diagram method is the key to the understanding of engineering problems. This is because the isolation of a body is the tool that clearly separates cause and effect and focuses our attention to the literal application of a principle. Example: Consider the book resting on the table in Figure 1. Although the book is stationary, two forces are acting on the book to keep it stationary. One is the weight (W) of the book exerting a force down on the table. The other is the force exerted up by the table to hold the book in place. This force is known as the normal force (N) and is equal to the weight of the book. A normal force is defined as any perpendicular force with which any two surfaces are pressed against each other. The free-body diagram for this situation, illustrated on the right side in Figure 1, isolates the book and presents the forces acting on the object. FREE-BODY DIAGRAMS Application of Newton's Laws CP-04 Page 6 Rev. 0 Figure 1 Book on a Table Constructing a Free-Body Diagram In constructing a free-body diagram the following steps are usually followed. Step 1. Determine which body or combination of bodies is to be isolated. The body chosen will usually involve one or more of the desired unknown quantities. Step 2. Next, isolate the body or combination of bodies chosen with a diagram that represents its complete external boundaries. Step 3. Represent all forces that act on the isolated body as applied by the removed contacting and attracting bodies in their proper positions in the diagram of the isolated body. Do not show the forces that the object exerts on anything else, since these forces do not affect the object itself.

Step 4. Indicate the choice of coordinate axes directly on the diagram. Pertinent dimensions may also be represented for convenience. Note, however, that the free-body diagram serves the purpose of focusing accurate attention on the action of the external forces; therefore, the diagram should not be cluttered with excessive information. Force arrows should be clearly distinguished from other arrows to avoid confusion. For this purpose colored pencils may be used. Application of Newton's Laws FREE-BODY DIAGRAMS Rev. 0 Page 7 CP-04 Figure 2 Car When these steps are completed a correct free-body diagram will result, and the student can apply the appropriate equations to the diagram to find the proper solution. Example: The car in Figure 2 is being towed by a force of some magnitude. Construct a free-body diagram showing all the forces acting on the car. Solution: Following the steps to construct a free-body diagram (shown in Figure 3), the object (the car) is chosen and isolated. All the forces acting on the car are represented with proper coordinate axes. Those forces are: F - The force applied to tow the carapp F - The frictional force that opposes the applied force due to theK weight of the car and the nature of the surfaces (the car's tires and the road) W - The weight of the car N - The normal force exerted by the road on the car FREE-BODY DIAGRAMS Application of Newton's Laws CP-04 Page 8 Rev. 0 Figure 3 Free-Body Diagram The frictional force (F ) is a force that opposes the direction of motion. This force isK explained in more detail in the chapter on types of forces. To solve this practical problem, the student would assign values for each force as determined by data given in the problem. After assigning a sign convention (e.g., + for forces upward and to the right, - for forces downward and to the left), the student would sum all forces to find the net force acting on the body. Using this net force information and appropriate equations, the student could solve for the requested unknowns. A variation would be to have the student find an unknown force acting on the body given sufficient information about the other forces acting on the body. The student will learn to solve specific examples using free-body diagrams in a later chapter. Some advanced free-body diagrams for various types of systems are shown in Figure 4. Application of Newton's Laws FREE-BODY DIAGRAMS Rev. 0 Page 9 CP-04 Figure 4 Various Free-Body Diagrams FREE-BODY DIAGRAMS Application of Newton's Laws CP-04 Page 10 Rev. 0 Free-Body Diagram Summary C A free-body diagram isolates a body and illustrates all the forces that act on the body so that a complete and accurate account of all of those forces may be considered. C Four steps must be performed to construct a free-body diagram: - Determine the body or combination of bodies to be isolated. - Isolate the body or combination of bodies with a diagram that represents the complete external boundaries. - Represent all forces that act on the isolated body in their proper positions within the diagram. - Indicate the choice of coordinate axes directly on the diagram. Summary The concept of the free-body diagram is summarized below. Application of Newton's Laws FORCE EQUILIBRIUM Rev. 0 Page 11 CP-04 FORCE EQUILIBRIUM Knowledge of the forces required to maintain an object in equilibrium is essential in understanding the nature of bodies at rest and in motion.

EO 1.4 STATE the conditions necessary for a body to be in force equilibrium. EO 1.5 DEFINE the following: a. Net force b. Equilibrant Net Force When forces act on an object, the result may be a change in the object's state of motion. If certain conditions are satisfied, however, the forces may combine to maintain a state of equilibrium or balance. To determine if a body is in equilibrium, the overall effect of all the forces acting on it must be assessed. All the forces that act on an object result in essentially one force that influences the object's motion. The force which results from all the forces acting on a body is defined as the net force. It is important to remember that forces are vector quantities. When analyzing various forces you must account for both the magnitude (displacement) of the force as well as the direction in which the force is applied. As described in the previous chapter, this is best done using a free-body diagram. To understand this more clearly, consider the book resting on the table in section A of Figure 5. FORCE EQUILIBRIUM Application of Newton's Laws CP-04 Page 12 Rev. 0 Figure 5 Net Force The book remains stationary resting on the table because the table exerts a normal force upward equal to the weight of the book. Therefore, the net force on the book is zero. If a force is applied to the book (section B of Figure 5), and the effect of friction is neglected, the net force will be equal to the applied force, and the book will move in the direction of the applied force. The free-body diagram in section C of Figure 5 shows that the weight (W) of the book is canceled by the normal force (N) of the table since they are equal in magnitude but opposite in direction. The resultant (net) force is therefore equal to the applied force (F ).APP Equilibrium Since an object in equilibrium is considered to be in a state of balance, it can be surmised that the net force on the object is equal to zero. That is, if the vector sum of all the forces acting on an object is equal to zero, then the object is in equilibrium. Newton's first law of motion describes equilibrium and the effect of force on a body that is in equilibrium. That law states "An object remains at rest (if originally at rest) or moves in a straight line with a constant velocity if the net force on it is zero." Newton's first law of motion is also called the law of inertia. Inertia is the tendency of a body to resist a change in its state of motion. F1 % F2 % F3 ' 0 'F ' 0 'FX ' 0 'FY ' 0 'FZ ' 0 Application of Newton's Laws FORCE EQUILIBRIUM Rev. 0 Page 13 CP-04 Figure 6 Hanging Object The first condition of equilibrium, a consequence of Newton's first law, may be written in vector form, "A body will be in translational equilibrium if and only if the vector sum of forces exerted on a body by the environment equals zero." For example, if three forces act on a body it is necessary for the following to be true for the body to be in equilibrium. (4-3) This equation may also be written as follows. (4-4) This sum includes all forces exerted on the body by its environment. The vanishing of this vector sum is a necessary condition, called the first condition of equilibrium, that must be satisfied in order to ensure translational equilibrium. In three dimensions (x,y,z), the component equations of the first condition of equilibrium are: (4-5) This condition applies to objects in motion with constant velocity and to bodies at rest or in static equilibrium (referred to as STATICS).

Applying the knowledge that an object in equilibrium has a net force equal to zero, the following example can be solved: Example: The object in Figure 6 has a weight of 125 lbf. The object is suspended by cables as shown. Calculate the tension (T ) in the cable at 30E with1 the horizontal. 'Fx ' T1x % T2x % T3x ' 0 'Fy ' T1y % T2y % T3y ' 0 'Fy ' (T1 sin30E) % (T2 sin180E) % (T3 sin270E) ' 0 (T1)(0.5) % (T2)(0) % (125 lbf)(&1) ' 0 0.5T1 & 125 lbf ' 0 0.5T1 ' 125 lbf T1 ' 250 lbf FORCE EQUILIBRIUM Application of Newton's Laws CP-04 Page 14 Rev. 0 Figure 7 Free-Body Diagram The tension in a cable is the force transmitted by the cable. The tension at any point in the cable can be measured by cutting a suitable length from it and inserting a spring scale. Solution: Since the object and its supporting cables are motionless (i.e., in equilibrium), we know that the net force acting on the intersection of the cables is zero. The fact that the net force is zero tells us that the sum of the x-components of T , T , and T is zero, and the1 2 3 sum of the y-components of T , T , and T is zero.1 2 3 The tension T is equal to the weight of the object, 125 lbf. The x and y components of the3 tensions can be found using trigonometry (e.g., sine function). Substituting known values into the second equation above yields the following. A simpler method to solve this problem involves assigning a sign convention to the free-body diagram and examining the direction of the forces. j F y ' (T 1 sin 30 E) & 125 lbf ' 0 0.5 T 1 ' 125 lbf T 1 ' 250 lbf j Forces' F1 % F2 % N % W ' 0 Application of Newton's Laws FORCE EQUILIBRIUM Rev. 0 Page 15 CP-04 Figure 8 Free-Body Diagram By choosing (+) as the upward direction and (-) as the downward direction, the student can determine by examination that 1) the upward component of T is + T sin 30 , 2) the tension T1 1 3 o is -125 lbf, and 3) T has no y- component. Therefore, using the same equation as before, we2 obtain the following. If the sum of all forces acting upon a body is equal to zero, that body is said to be in force equilibrium. If the sum of all the forces is not equal to zero, any force or system of forces capable of balancing the system is defined as an equilibrant. Example: A 2000 lbm car is accelerating (on a frictionless surface) at a rate of 2 ft-sec. What force must be applied to the car to act as an equilibrant for this system? Solution: a. Draw a free-body diagram. b. A Force, F , MUST be applied in the opposite direction to F such that the2 1 sum of all forces acting on the car is zero. F2 ' F1 ' ma gc ' (2000 lbm × 2ft&sec2) ÷ 32.17 ft&lbm lbf&sec2 ' 124 lbf FORCE EQUILIBRIUM Application of Newton's Laws CP-04 Page 16 Rev. 0 Force Equilibrium Summary C The force that is the resultant force of all forces acting on a body is defined as the net force. C If the vector sum of all the forces acting on an object is equal to zero, then the object is in equilibrium. C The first condition of equilibrium is stated as follows: "A body will be in translational equilibrium if and only if the vector sum of forces exerted on a body by the environment equals zero." F + F + F = 01 2 3 or 'F = 0 C Any force or system of forces capable of balancing a system so that the net force is zero is defined as an equilibrant. c. Since the car remains on the surface, forces N and W are in equal and opposite directions. Force F must be applied in an equal and opposite2

direction to F in order for the forces to be in equilibrium.1 Summary The concepts presented in this chapter are summarized below. Application of Newton's Laws TYPES OF FORCE Rev. 0 Page 17 CP-04 TYPES OF FORCE When determining how an object reacts to a force or forces, it is important to understand the different types of forces that may act on the object. EO 1.6 DEFINE the following: a. Tensile force b. Compressive force c. Frictional force EO 1.7 EXPLAIN the difference between a static-friction force and a kinetic-friction force. EO 1.8 STATE two factors that affect the magnitude of the friction force. EO 1.9 EXPLAIN the difference between centripetal force and centrifugal force. The previous section discussed the equilibrium of forces as they act on bodies. Recalling that a force is defined as a vector quantity that tends to produce an acceleration of a body in the direction of its application, it is apparent that the student must be acquainted with the various types of forces that exist in order to construct a correct free-body diagram and apply the appropriate equation. A force is applied either by direct mechanical contact or by remote action. Tensile and Compressive Forces In discussing the types of forces, a simple rule is used to determine if the force is a tensile or a compressive force. If an applied force on a member tends to pull the member apart, it is said to be in tension. If a force tends to compress the member, it is in compression. It should also be mentioned that ropes, cables, etc., that are attached to bodies can only support tensile loads, and therefore such objects are in tension when placed on the free-body diagram. In addition, when a fluid is involved, it should be understood that fluid forces are almost always compressive forces. Friction Another type of force often used in classical physics is the force resulting from two surfaces in contact, where one of the surfaces is attempting to move parallel to or over the other surface. Such forces are referred to as friction forces. There are two types of friction forces: those due to dry friction, sometimes called Coulomb friction, and those resulting from fluid friction. TYPES OF FORCE Application of Newton's Laws CP-04 Page 18 Rev. 0 Figure 9 Frictional Forces Fluid friction develops between layers of fluid moving at different velocities. This type of frictional force is used in considering problems involving the flow of fluids through pipes. Such problems are covered in the Fundamentals Manual on fluid flow. In this section, problems involving rigid bodies which are in contact along dry surfaces are considered. The laws of dry friction are best understood by the following experiment. A block of weight W is placed on a horizontal plane surface (see Figure 9). The forces acting on the block are its weight W and the normal force N of the surface. Since the weight has no horizontal component, the normal force of the surface also has no horizontal component; the reaction is therefore normal to the surface and is represented by N in part (a) of the figure. Suppose now, that a horizontal force P is applied to the block (see part (b)). If P is small, the block will not move. Some other horizontal force must therefore exist which balances P. This other force is the static-friction force F, which is actually the resultant of a great number of forces acting over the entire surface of contact between the block and the plane. The nature of these forces is not known exactly, but it is generally assumed that these forces are due to the irregularities of the surfaces in contact and also to molecular action.

If the force P is increased, the friction force F also increases, continuing to oppose P, until its magnitude reaches a certain maximum value F (see part (c) of Figure 9). If P is further increased,M the friction force cannot balance it any more, and the block starts sliding. As soon as the block has been set in motion, the magnitude of F drops from F to a lower value F . This is because there isM K less interpenetration between the irregularities of the surfaces in contact when these surfaces move with respect to one another. From then on, the block keeps sliding with increasing velocity (i.e., it accelerates) while the friction force, denoted by F and called the kinetic-friction force, remainsK approximately constant. FM ' µs N FK ' µK N Application of Newton's Laws TYPES OF FORCE Rev. 0 Page 19 CP-04 Figure 10 Centripetal Force Experimental evidence shows that the maximum value F of the static-friction force isM proportional to the normal component N of the reaction of the surface, as shown in Equation 4-5. (4-5) The term µ is a constant called the coefficient of static friction. Similarly, the magnitude F ofs K the kinetic-friction force may be expressed in the following form. (4-6) The term µ is a constant called the coefficient of kinetic friction. The coefficients of friction,K µ and µ , do not depend upon the area of the surfaces in contact. Both coefficients, however,S K depend strongly on the nature of the surfaces in contact. Since they also depend upon the exact condition of the surfaces, their value is seldom known with an accuracy greater than 5 percent. It should be noted that frictional forces are always opposite in direction to the motion (or impending motion) of the object. Centripetal Force An object moving at constant speed in a circle is not in equilibrium. Although the magnitude of the linear velocity is not changing, the direction of velocity is continually changing. Since a change in direction requires acceleration, an object moving in a circular path has a constant acceleration towards the center of the circular path. Recalling Newton's second law of motion, F = ma, a force is required to cause acceleration. Therefore, to have constant acceleration towards the center of the circular path, there must be a net force acting towards the center. This force is known as centripetal force. Without this force, an object will move in a straight line. Figure 10 illustrates the centripetal force. TYPES OF FORCE Application of Newton's Laws CP-04 Page 20 Rev. 0 Figure 11 Centrifugal Force Figure 12 Loss of Centripetal Force Centrifugal Force Another force, which appears to be opposite the direction of motion, is the centrifugal force acting on an object that follows a curved path. This force appears to be a force directed away from the center of the circular path. This is actually a fictitious force, but is an apparent force that is used to describe the forces present due to an object's rotation. To better understand centripetal and centrifugal forces, consider that a string is attached to the plane in Figure 10. As the plane rotates about the center, the string places a centripetal force on the plane. This causes the plane's velocity to change in direction, thus causing it to travel in a circle.

The apparent outward force, centrifugal force, seems to pull the plane away from the center shown in Figure 11. This is the same apparent outward force one feels when riding in a car when the car travels in a circle. It can be proven that centrifugal force is not an actual force by cutting the string. In doing so, the plane will fly off in a straight line that is tangent to the circle at the velocity it had the moment the string was cut. If there were an actual centrifugal force present, the plane would not fly away in a line tangent to the circle, but would fly directly away from the circle (see Figure 12). Application of Newton's Laws TYPES OF FORCE Rev. 0 Page 21 CP-04 Types of Force Summary C A tensile force is an applied force that tends to pull an object apart. C A compressive force is an applied force that tends to compress an object. C Frictional force is the force resulting from two surfaces in contact, where one of the surfaces is attempting to move with respect to the other surface. C Static-frictional forces are those frictional forces present when an object is stationary, whereas kinetic-frictional forces are those frictional forces present between two objects that are moving. C The magnitude of the frictional force is affected by the following: - Weight of the object being moved - Type of surface on the object being moved - Type of surface on which the object is moving. C Centripetal force is the force on an object moving in a circular path that is directed towards the center of the path, whereas the centrifugal force is the fictitious force that appears to be directed away from the center of the circular path. Summary The concepts of this chapter are summarized below. Application of Newton's Laws CP-04 Page 22 Rev. 0 Intentionally Left Blank Department of Energy Fundamentals Handbook CLASSICAL PHYSICS Module 5 Energy, Work, and Power Energy, Work and Power TABLE OF CONTENTS Rev. 0 Page i CP-05 TABLE OF CONTENTS LIST OF FIGURES. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ii LIST OF TABLES. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . iii REFERENCES. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . iv OBJECTIVES. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . v ENERGY AND WORK. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 Energy . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 Potential Energy. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1 Kinetic Energy . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 Thermal Energy. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 Mechanical Energy. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3 Work . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 Summary . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5

LAW OF CONSERVATION OF ENERGY. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6 Conservation of Energy. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6 Summary . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7 POWER. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8 Power. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8 Thermal Power. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8 Mechanical Power. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9 Summary . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11 LIST OF FIGURES Energy, Work, and Power CP-05 Page ii Rev. 0 LIST OF FIGURES NONE Energy, Work, and Power LIST OF TABLES Rev. 0 Page iii CP-05 LIST OF TABLES NONE REFERENCES Energy, Work, and Power CP-05 Page iv Rev. 0 REFERENCES C Beiser, Arthur, Applied Physics Schaums Outline Series, McGraw-Hill Book Company, 1976. C Murray, Raymond and Cobb, Grover, Physics Concepts and Consequences, Prentice-Hall, Inc., 1970. C Alexander, Joseph, et al., Physics for Engineering Technology, John Wiley and Sons, 1978. C Sears, Francis and Zemansky, Mark, University Physics, 3rd edition, Addison- Wesley Publishing Co. C Science and Fundamental Engineering (SAFE), Classical Physics, "Measure" Combustion Engineering, Inc., 1988. C Academic Program for Nuclear Power Plant Personnel, Volume II, General Physics Corporation, Library of Congress Card #A 397747, April 1982. Energy, Work, and Power OBJECTIVES Rev. 0 Page v CP-05 TERMINAL OBJECTIVE 1.0 Given necessary information about a system, CALCULATE the work performed and/or power produced or used by that system. ENABLING OBJECTIVES 1.1 DEFINE the following terms: a. Energy b. Potential energy c. Kinetic energy d. Work e. Power 1.2 STATE the mathematical expression for: a. Potential energy b. Kinetic energy c. Work d. Power 1.3 For a mechanical system, CALCULATE energy, work, and power. 1.4 STATE the First Law of Thermodynamics, "Conservation of Energy." Energy, Work, and Power CP-05 Page vi Rev. 0 Intentionally Left Blank Energy, Work, and Power ENERGY AND WORK Rev. 0 Page 1 CP-05 ENERGY AND WORK Energy is the measure of the ability to do work or cause a change. Work is a measure of the amount of energy required to move an object. EO 1.1 DEFINE the following terms: a. Energy b. Potential energy c. Kinetic energy d. Work EO 1.2 STATE the mathematical expression for: a. Potential energy b. Kinetic energy c. Work EO 1.3 For a mechanical system, CALCULATE energy, work, and power. Energy Energy is defined as the measure of the ability to do work. Energy determines the capacity of a system to perform work and may be stored in various forms. Some of the more basic mechanical systems involve the concepts of potential and kinetic energy. Both of these terms will be explained more fully later in this chapter. More advanced systems may include other types of energy such as chemical, electromagnetic, thermal, acoustic, and nuclear. A piledriver hammer performs work by virtue of its falling motion. Coal burned in a fossil-fueled power plant is undergoing energy release by a chemical reaction. Fuel elements in a nuclear power reactor produce energy by a nuclear reaction. For the purposes of this course, our discussions will be limited to mechanical and thermal forms of energy (e.g., heat). It should be noted, however, that the principles involved with energy calculations are similar for all types of energy.

Both thermal and mechanical energy can be separated into two categories, transient and stored. Transient energy is energy in motion, that is, energy being transferred from one place to another. Stored energy is the energy contained within a substance or object. Both of these categories of energy will be discussed in this module. Potential Energy Potential energy is defined as the energy stored in an object because of its position. An example is the potential energy of an object above the surface of the earth in the earth's gravitational field. Potential energy also applies to energy due to separation of electrical charge and to energy stored in a spring, in other words, energy due to position of any force field. ' mgz gc PE ' mgz gc ' 50 lbm 1 32.17 ft sec2 10 ft 1 lbf&sec2 32.17 lbm&ft KE ' mv2 2gc ENERGY AND WORK Energy, Work, and Power CP-05 Page 2 Rev. 0 As an example, consider the energy stored in hydrogen and oxygen as potential energy to be released on burning. Burning changes their relative separation distance from the elemental form to the compound form as water releases the potential energy. When discussing mechanical potential energy, we look at the position of an object. The measure of an object's position is its vertical distance above a reference point. The reference point is normally the earth's surface, but can it be any point. The potential energy of the object represents the work required to elevate the object to that position from the reference point. Potential energy is mathematically represented by Equation 5-1. PE = work to elevate = weight x height (5-1) where: PE = potential energy in ft-lbf m = mass in lbm g = 32.17 ft/sec2 g = 32.17 (lbm-ft)/(lbf-sec )c 2 z = height above a reference in ft It should be noted the g is used only when using the English system of measurement.c Example: What is the potential energy of a 50 lbm object suspended 10 feet above the ground? Answer: PE = 500 ft-lbf Kinetic Energy Kinetic energy is defined as the energy stored in an object because of its motion. If you have a baseball in your hand, it has no kinetic energy because it is not moving. But if you throw the ball, your hand has provided energy to give the ball motion. When you release the ball, it leaves your hand at some velocity. The energy you have given the ball will determine the velocity of the ball. Because the kinetic energy is due to the motion of the object, and motion is measured by velocity, kinetic energy can be calculated in terms of its velocity, as shown below. (5-2) KE ' mv2 2gc ' 10 lbm 2 8 ft sec 2 lbf&sec2 32.17 lbm&ft KE ' (5 lbm) 64 ft2 sec2 lbf&sec2 32.17 lbm&ft Energy, Work, and Power ENERGY AND WORK Rev. 0 Page 3 CP-05 where: KE = kinetic energy in ft-lbf m = mass in lbm v = velocity in ft/sec g = (32.17 lbm-ft)/(lbf-sec )c 2 Example: What is the kinetic energy of a 10 lbm object that has a velocity of 8 ft/sec? Answer: KE = 9.95 ft-lbf The kinetic energy of an object represents the amount of energy required to increase the velocity of the object from rest (v = 0) to its final velocity, or the work it can do as it pushes against something in slowing down (waterwheel or turbine, for example.) Thermal Energy

Thermal energy is that energy related to temperature (the higher the temperature, the greater the molecular movement, and the greater the energy). If one object has more thermal energy than an adjacent substance, the substance at the higher temperature will transfer thermal energy (at a molecular level) to the other substance. Note that the energy is moving from one place to another (it is in motion) and is referred to as transient energy or, more commonly in the case of thermal energy, heat. The only stored energy in a solid material is internal energy. Internal energy is the energy stored in a substance because of the motion and position of the particles of the substance. Heat and internal energy will be covered in the Fundamentals Manual on Heat Transfer, Fluid Flow, and Thermodynamics. Mechanical Energy Mechanical energy is energy related to motion or position. Transient mechanical energy is commonly referred to as work. Stored mechanical energy exists in one of two forms: kinetic or potential. Kinetic and potential energy can be found in both fluids and solid objects. ENERGY AND WORK Energy, Work, and Power CP-05 Page 4 Rev. 0 Work Work is commonly thought of as any activity requiring exertion. However, the definition in physics is much more specific. Work is done by a force acting on a moving object if the object has some component of motion in the direction of the force. Work can be done BY a person, a machine, or an object by applying a force and causing something to move. More specifically, work is done by a force acting on a moving object if the object has some component of motion in the direction of the force. Work can be done ON an object by applying a force that causes it to move. For example, if you push on a box (apply a force) and it moves three feet, work has been performed BY you to the box, while work has been performed ON the box. If you push on the box and it does not move, then work, by our definition, has not been accomplished. Work can be defined mathematically by Equation 5-3. W = F x d (5-3) where: W = work done in ft-lbf F = force applied to the object in lbf d = distance the object is moved (in ft.) with the force applied Example: You push a large box for three minutes. During that time, you exert a constant force of 200 lbf to the box, but it does not move. How much work has been accomplished? W = F x d W = 200 lbf x 0 ft W = 0 ft-lbf work done Remember that if no movement is achieved, no work has been accomplished. Even if you feel fatigued, no work has been done. Work can be thought of as what has been accomplished. If nothing is accomplished, then no work has been done. Example: You push the same box as mentioned above. You apply a horizontal force of 200 lbf to the box, and the box moves five feet horizontally. How much work have you done? W = F x d W = 200 lbf x 5 ft W = 1000 ft-lbf In this case, work can be described as work done by the person pushing the box or work performed on the box. In either case, the amount of work is the same. KE ' mv2 2gc 1 2 mv2 PE ' mgz gc Energy, Work, and Power ENERGY AND WORK Rev. 0 Page 5 CP-05 Summary The main points covered in this chapter are summarized below. Energy and Work Summary C Energy is the ability to do work. C The work done by a force on an object is the product of the force and the distance the object moves in the direction of the force. C Kinetic energy is the energy an object has because of its motion.

C or KE = C Potential energy is the energy of an object due to its position. C LAW OF CONSERVATION OF ENERGY Energy, Work, and Power CP-05 Page 6 Rev. 0 LAW OF CONSERVATION OF ENERGY Energy does not simply appear and disappear. Energy is transferred from one position to another or transformed from one type of energy to another. EO 1.4 STATE the First Law of Thermodynamics, "Conservation of Energy." Conservation of Energy The First Law of Thermodynamics is simply stated "energy cannot be created or destroyed, only altered in form." In the previous chapter, we discussed potential energy, where a force is applied to an object, raising it from some point of origin to some height. The energy expended in raising the object is equivalent to the potential energy gained by the object because of its height. This is an example of a transfer of energy as well as an alteration of the type of energy. Another example is throwing a baseball. While the ball is in your hand, it contains no kinetic energy. You apply a force to the ball by throwing it. The ball leaves your hand with a velocity, giving it kinetic energy equal to the work applied by your hand. Mathematically, this can be described by the following simplified equation. Energy + Energy - Energy = Energy (5-4)initial added removed final where: Energy is energy initially stored in an object/substance. This energy can exist ininitial various combinations of kinetic energy and potential energy. Energy is energy added to the object/substance. Heat can be added. Energy can beadded added in the form of stored energy in any mass added, such as water to a fluid system. Work can be done on a system. Heat is energy gained or lost at a microscopic level. Work is the same at a macroscopic level. Energy is energy removed from an object/substance. Heat can be rejected. Workremoved can be done by the system. This energy can be in the form of energy stored in any mass removed. Energy is energy remaining within the object/substance after all energy transfers andfinal transformations occur. This energy can exist in various combinations of kinetic, potential, flow, and internal energy. Energy, Work, and Power LAW OF CONSERVATION OF ENERGY Rev. 0 Page 7 CP-05 Conservation of Energy Summary C Energy cannot be created or destroyed, only altered in form. C Simplified energy balance: KE + PE + E = KE + PE + E1 1 added 2 2 removed To further describe each of the components of the above equation, each component can be broken down as follows: Energy = KE + PEinitial 1 1 Energy = Work done on and heat added to the systemadded Energy = Work done by and heat removed from the systemremoved Energy = KE + PEfinal 2 2 The resulting energy balance is provided in Equation 5-5. KE + PE + E - E = KE + PE (5-5)1 1 added removed 2 2 Neglecting any heat removed or added to a system, we can replace E and E inadded removed Equation 5-5 with their associated work terms to obtain Equation 5-6. KE + PE + W = KE + PE + W (5-6)1 1 on 2 2 by The final energy balance is called a "simplified energy balance." Any energy balance is a statement of the Law of Conservation of Energy. In this simplified form, the balance applies only to mechanical problems, since we neglected heat. However, more specific energy balances that include heat will be discussed in other Fundamental Manuals. For example, specific energy balances for flow systems will be discussed in the Heat Transfer, Fluid Flow, and Thermodynamics modules.

Summary The law of conservation of energy is summarized below. Thermal Power' heat used time required POWER Energy, Work, and Power CP-05 Page 8 Rev. 0 POWER Power is a measure of the rate at which energy is used. Thermal power is the term used to refer to the transfer of heat. Mechanical power is the term used to describe when work is being done. EO 1.1 DEFINE the following terms: e. Power EO 1.2 STATE the mathematical expression for: d. Power EO 1.3 For a mechanical system, CALCULATE energy, work, and power. Power Power is defined as the amount of energy used per unit time or rate of doing work. It has the units of watt, Btu, horsepower, or ft-lbf/sec. Thermal Power Thermal power is the measure of thermal energy used per unit time. It is the rate of heat transfer or heat flow rate. Examples of thermal power units are British Thermal Units (Btu) or kilowatts (Kw). Thermal power is calculated basically by the mathematical expression of: Thermal energy and calculations of thermal power will be covered in more detail in the Fundamentals Manual for Heat Transfer, Fluid Flow, and Thermodynamics. Power' work done time required P ' Fd t P ' Fv 550 Energy, Work, and Power POWER Rev. 0 Page 9 CP-05 Mechanical Power Mechanical energy used per unit time is called mechanical power. Mechanical power is the rate at which work is done. Mechanical power is expressed in units of joules/sec (joules/s) or a watt (W) in the mks system, and feet - pounds force per second (ft-lbf/s) or horsepower (hp) in the English system. Mechanical power can be calculated using the following mathematical expression. Because work can be defined as force times distance, we can also use the following equation: (5-6) where: P = Power (W or ft-lbf/s) F = Force (N or lbf) d = distance (m or ft) t = time (sec) One horsepower is equivalent to 550 ft-lbf/s and 745.7 watts. Because in the equation above d divided by t is the same as velocity, an alternate description of power is as follows. (5-7) where: P = power (hp) F = force (lbf) v = velocity (ft/s) When using equations 5-6 or 5-7, you must either assume force and velocity are constant or that average values of the force and velocity are used. Power' work done time required P ' 1.5 x 108 ft&lbf 100 min 1 min 60 sec 1 hp 550 ft&lbf/sec P ' 45.5 hp P ' Fv 550 P ' (1 lbf) (5 ft/sec) 550 P ' 9 x 10&3 hp POWER Energy, Work, and Power CP-05 Page 10 Rev. 0 Example 1: A pump provides a flow rate of 10,000 gpm. The pump does 1.5 x 10 ft-lbf of work8 every 100 minutes. What is the power of the pump in hp? Example 2: A boy rolls a ball with a steady force of 1 lbf, giving the ball a constant velocity of 5 ft/s. What is the power used by the boy in rolling the ball? P ' Fd t P ' (1890 lbf)(1455 ft) 5 sec 1 hp 550 ft&lbf/sec P ' 1000 hp P ' Fv 550 P ' (1890 lbf)(291 ft/sec) 550 P ' 1000 hp Power' work done time required Energy, Work, and Power POWER Rev. 0 Page 11 CP-05 Example 3: A race car traveling at constant velocity can go one quarter mile (1455 ft) in 5 seconds. If the motor is generating a force of 1890 lbf pushing the car, what is the power of the motor in hp? Assume the car is already at full speed at t=0. or Summary The main points of this chapter are summarized below. Power Summary C Power is the amount of energy used per unit time. C POWER Energy, Work, and Power CP-05 Page 12 Rev. 0 end of text. CONCLUDING MATERIAL Review activities: Preparing activity: DOE - ANL-W, BNL, EG&G Idaho, DOE - NE-73 EG&G Mound, EG&G Rocky Flats, Project Number 6910-0016 LLNL, LANL, MMES, ORAU, REECo, WHC, WINCO, WEMCO, and WSRC. ABSTRACT