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Vote # Introduction to Thermodynamics and Heat Transfer: Solutions Manual (PDF)

2008 • 1,312 Pages • 9.03 MB • English
Posted April 14, 2020 • Submitted by schaefer.flavio

## Summary of Introduction to Thermodynamics and Heat Transfer: Solutions Manual

1-1 Solutions Manual for Introduction to Thermodynamics and Heat Transfer Yunus A. Cengel nd 2 Edition, 2008 Chapter 1 INTRODUCTION AND OVERVIEW PROPRIETARY AND CONFIDENTIAL This Manual is the proprietary property of The McGraw-Hill Companies, Inc. (“McGraw-Hill”) and protected by copyright and other state and federal laws. By opening and using this Manual the user agrees to the following restrictions, and if the recipient does not agree to these restrictions, the Manual should be promptly returned unopened to McGraw-Hill: This Manual is being provided only to authorized professors and instructors for use in preparing for the classes using the affiliated textbook. No other use or distribution of this Manual is permitted. This Manual may not be sold and may not be distributed to or used by any student or other third party. No part of this Manual may be reproduced, displayed or distributed in any form or by any means, electronic or otherwise, without the prior written permission of McGraw-Hill. PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.

1-2 Thermodynamics, Heat Transfer, and Fluid Mechanics 1-1C Classical thermodynamics is based on experimental observations whereas statistical thermodynamics is based on the average behavior of large groups of particles. 1-2C On a downhill road the potential energy of the bicyclist is being converted to kinetic energy, and thus the bicyclist picks up speed. There is no creation of energy, and thus no violation of the conservation of energy principle. 1-3C There is no truth to his claim. It violates the second law of thermodynamics. 1-4C A car going uphill without the engine running would increase the energy of the car, and thus it would be a violation of the first law of thermodynamics. Therefore, this cannot happen. Using a level meter (a device with an air bubble between two marks of a horizontal water tube) it can shown that the road that looks uphill to the eye is actually downhill. 1-5C Thermodynamics deals with the amount of heat transfer as a system undergoes a process from one equilibrium state to another. Heat transfer, on the other hand, deals with the rate of heat transfer as well as the temperature distribution within the system at a specified time. 1-6C (a) The driving force for heat transfer is the temperature difference. (b) The driving force for electric current flow is the electric potential difference (voltage). (a) The driving force for fluid flow is the pressure difference. 1-7C Heat transfer is a non-equilibrium phenomena since in a system that is in equilibrium there can be no temperature differences and thus no heat flow. 1-8C No, there cannot be any heat transfer between two bodies that are at the same temperature (regardless of pressure) since the driving force for heat transfer is temperature difference. 1-9C The absolute minimum energy needed to move this car horizontally is zero since the acceleration is zero. Note that Force = mass × acceleration and Work = Force × distance. PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.

1-3 Mass, Force, and Units 1-10C Pound-mass lbm is the mass unit in English system whereas pound-force lbf is the force unit. One 2 pound-force is the force required to accelerate a mass of 32.174 lbm by 1 ft/s . In other words, the weight of a 1-lbm mass at sea level is 1 lbf. 1-11C In this unit, the word light refers to the speed of light. The light-year unit is then the product of a velocity and time. Hence, this product forms a distance dimension and unit. 1-12C There is no acceleration, thus the net force is zero in both cases. 1-13E The weight of a man on earth is given. His weight on the moon is to be determined. Analysis Applying Newton's second law to the weight force gives 2 W 180 lbf ⎛ 32.174 lbm ⋅ft/s ⎞ W = mg ⎯⎯→m = = ⎜ ⎟ =180.4 lbm 2 ⎜ ⎟ g 32.10 ft/s ⎝ 1 lbf ⎠ Mass is invariant and the man will have the same mass on the moon. Then, his weight on the moon will be 2 ⎛ 1 lbf ⎞ W = mg = (180.4 lbm)(5.47 ft/s )⎜ ⎟ = 30.7 lbf 2 ⎝ 32.174 lbm⋅ft/s ⎠ 1-14 The interior dimensions of a room are given. The mass and weight of the air in the room are to be determined. Assumptions The density of air is constant throughout the room. 3 Properties The density of air is given to be ρ = 1.16 kg/m . Analysis The mass of the air in the room is ROOM AIR 3 3 m = ρV = (1.16 kg/m )(6×6×8 m ) = 334.1 kg 3 6X6X8 m Thus, 2 ⎛ 1 N ⎞ W = mg = (334.1 kg)(9.81 m/s )⎜ ⎟ = 3277 N ⎜ 2 ⎟ 1 kg ⋅m/s ⎝ ⎠ PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.

1-4 1-15 The variation of gravitational acceleration above the sea level is given as a function of altitude. The height at which the weight of a body will decrease by 1% is to be determined. z Analysis The weight of a body at the elevation z can be expressed as −6 W = mg = m(9.807 − 3.32 ×10 z) In our case, W = 0.99W = 0.99mg = 0.99(m)(9.807) s s Substituting, 0 −6 0.99(9.81) = (9.81−3.32×10 z) ⎯⎯→ z = 29,539 m Sea level 1-16E The mass of an object is given. Its weight is to be determined. Analysis Applying Newton's second law, the weight is determined to be 2 ⎛ 1 lbf ⎞ W = mg = (10 lbm)(32.0 ft/s )⎜ ⎟ = 9.95 lbf 2 ⎝ 32.174 lbm⋅ ft/s ⎠ 1-17 The acceleration of an aircraft is given in g’s. The net upward force acting on a man in the aircraft is to be determined. Analysis From the Newton's second law, the force applied is 2 ⎛ 1 N ⎞ F = ma = m(6 g) = (90 kg)(6×9.81 m/s )⎜ ⎟ = 5297 N ⎜ 2 ⎟ 1 kg ⋅m/s ⎝ ⎠ 1-18 CD EES A rock is thrown upward with a specified force. The acceleration of the rock is to be determined. Analysis The weight of the rock is 2 ⎛ 1 N ⎞ W = mg = (5 kg)(9.79 m/s )⎜ ⎟ = 48.95 N ⎜ 2 ⎟ 1 kg ⋅m/s ⎝ ⎠ Then the net force that acts on the rock is F = F − F =150 − 48.95 =101.05 N net up down Stone From the Newton's second law, the acceleration of the rock becomes 2 F 101.05 N ⎛1 kg ⋅m/s ⎞ 2 a = = ⎜ ⎟ = 20.2 m/s ⎜ ⎟ m 5 kg 1 N ⎝ ⎠ PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.

1-5 1-19 EES Problem 1-18 is reconsidered. The entire EES solution is to be printed out, including the numerical results with proper units. Analysis The problem is solved using EES, and the solution is given below. W=m*g "[N]" m=5 [kg] g=9.79 [m/s^2] "The force balance on the rock yields the net force acting on the rock as" F_net = F_up - F_down"[N]" F_up=150 [N] F_down=W"[N]" "The acceleration of the rock is determined from Newton's second law." F_net=a*m "To Run the program, press F2 or click on the calculator icon from the Calculate menu" SOLUTION a=20.21 [m/s^2] F_down=48.95 [N] F_net=101.1 [N] F_up=150 [N] g=9.79 [m/s^2] m=5 [kg] W=48.95 [N] 1-20 Gravitational acceleration g and thus the weight of bodies decreases with increasing elevation. The percent reduction in the weight of an airplane cruising at 13,000 m is to be determined. 2 2 Properties The gravitational acceleration g is given to be 9.807 m/s at sea level and 9.767 m/s at an altitude of 13,000 m. Analysis Weight is proportional to the gravitational acceleration g, and thus the percent reduction in weight is equivalent to the percent reduction in the gravitational acceleration, which is determined from Δg 9.807 −9.767 %Reduction in weight = %Reduction in g = ×100 = ×100 = 0.41% g 9.807 Therefore, the airplane and the people in it will weight 0.41% less at 13,000 m altitude. Discussion Note that the weight loss at cruising altitudes is negligible. PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.

1-6 Modeling and Solving Engineering problems 1-21C The rating problems deal with the determination of the heat transfer rate for an existing system at a specified temperature difference. The sizing problems deal with the determination of the size of a system in order to transfer heat at a specified rate for a specified temperature difference. 1-22C The experimental approach (testing and taking measurements) has the advantage of dealing with the actual physical system, and getting a physical value within the limits of experimental error. However, this approach is expensive, time consuming, and often impractical. The analytical approach (analysis or calculations) has the advantage that it is fast and inexpensive, but the results obtained are subject to the accuracy of the assumptions and idealizations made in the analysis. 1-23C Modeling makes it possible to predict the course of an event before it actually occurs, or to study various aspects of an event mathematically without actually running expensive and time-consuming experiments. When preparing a mathematical model, all the variables that affect the phenomena are identified, reasonable assumptions and approximations are made, and the interdependence of these variables are studied. The relevant physical laws and principles are invoked, and the problem is formulated mathematically. Finally, the problem is solved using an appropriate approach, and the results are interpreted. 1-24C The right choice between a crude and complex model is usually the simplest model which yields adequate results. Preparing very accurate but complex models is not necessarily a better choice since such models are not much use to an analyst if they are very difficult and time consuming to solve. At the minimum, the model should reflect the essential features of the physical problem it represents. Solving Engineering Problems and EES 1-25C Despite the convenience and capability the engineering software packages offer, they are still just tools, and they will not replace the traditional engineering courses. They will simply cause a shift in emphasis in the course material from mathematics to physics. They are of great value in engineering practice, however, as engineers today rely on software packages for solving large and complex problems in a short time, and perform optimization studies efficiently. 1-26 EES Determine a positive real root of the following equation using EES: 3 0.5 2x – 10x – 3x = -3 Solution by EES Software (Copy the following line and paste on a blank EES screen to verify solution): 2*x^3-10*x^0.5-3*x = -3 Answer: x = 2.063 (using an initial guess of x=2) PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.

1-7 1-27 EES Solve the following system of 2 equations with 2 unknowns using EES: 3 2 x – y = 7.75 3xy + y = 3.5 Solution by EES Software (Copy the following lines and paste on a blank EES screen to verify solution): x^3-y^2=7.75 3*x*y+y=3.5 Answer x=2 y=0.5 1-28 EES Solve the following system of 3 equations with 3 unknowns using EES: 2x – y + z = 5 2 3x + 2y = z + 2 xy + 2z = 8 Solution by EES Software (Copy the following lines and paste on a blank EES screen to verify solution): 2*x-y+z=5 3*x^2+2*y=z+2 x*y+2*z=8 Answer x=1.141, y=0.8159, z=3.535 1-29 EES Solve the following system of 3 equations with 3 unknowns using EES: 2 x y – z = 1 0.5 x – 3y + xz = - 2 x + y – z = 2 Solution by EES Software (Copy the following lines and paste on a blank EES screen to verify solution): x^2*y-z=1 x-3*y^0.5+x*z=-2 x+y-z=2 Answer x=1, y=1, z=0 PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.

1-8 1-30E EES Specific heat of water is to be expressed at various units using unit conversion capability of EES. Analysis The problem is solved using EES, and the solution is given below. EQUATION WINDOW "GIVEN" C_p=4.18 [kJ/kg-C] "ANALYSIS" C_p_1=C_p*Convert(kJ/kg-C, kJ/kg-K) C_p_2=C_p*Convert(kJ/kg-C, Btu/lbm-F) C_p_3=C_p*Convert(kJ/kg-C, Btu/lbm-R) C_p_4=C_p*Convert(kJ/kg-C, kCal/kg-C) FORMATTED EQUATIONS WINDOW GIVEN Cp = 4.18 [kJ/kg-C] ANALYSIS kJ/kg–K Cp,1 = Cp · 1 · kJ/kg–C Btu/lbm–F Cp,2 = Cp · 0.238846 · kJ/kg–C Btu/lbm–R Cp,3 = Cp · 0.238846 · kJ/kg–C kCal/kg–C Cp,4 = Cp · 0.238846 · kJ/kg–C SOLUTION WINDOW C_p=4.18 [kJ/kg-C] C_p_1=4.18 [kJ/kg-K] C_p_2=0.9984 [Btu/lbm-F] C_p_3=0.9984 [Btu/lbm-R] C_p_4=0.9984 [kCal/kg-C] PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.

1-9 Review Problems 1-31 The weight of a lunar exploration module on the moon is to be determined. Analysis Applying Newton's second law, the weight of the module on the moon can be determined from W earth 4000 N 2 W = mg = g = (1.64 m/s ) = 669 N moon moon moon 2 g earth 9.8 m/s 1-32 The gravitational acceleration changes with altitude. Accounting for this variation, the weights of a body at different locations are to be determined. Analysis The weight of an 80-kg man at various locations is obtained by substituting the altitude z (values in m) into the relation −6 2 ⎛ 1N ⎞ W = mg = (80kg)(9.807 − 3.32×10 zm/s )⎜ ⎟ ⎜ 2 ⎟ 1kg ⋅ m/s ⎝ ⎠ -6 Sea level: (z = 0 m): W = 80×(9.807-3.32x10 ×0) = 80×9.807 = 784.6 N -6 Denver: (z = 1610 m): W = 80×(9.807-3.32x10 ×1610) = 80×9.802 = 784.2 N -6 Mt. Ev.: (z = 8848 m): W = 80×(9.807-3.32x10 ×8848) = 80×9.778 = 782.2 N 1-33E A man is considering buying a 12-oz steak for \$3.15, or a 320-g steak for \$2.80. The steak that is a better buy is to be determined. Assumptions The steaks are of identical quality. Analysis To make a comparison possible, we need to express the cost of each steak on a common basis. Let us choose 1 kg as the basis for comparison. Using proper conversion factors, the unit cost of each steak is determined to be 12 ounce steak: ⎛ \$3.15 ⎞ ⎛16 oz ⎞ ⎛ 1 lbm ⎞ Unit Cost = ⎜ ⎟ ⎜ ⎟ ⎜ ⎟ = \$9.26/kg ⎜ ⎟ ⎝ 12 oz ⎠ ⎝1 lbm ⎠ ⎝ 0.45359 kg ⎠ 320 gram steak: ⎛ \$2.80 ⎞ ⎛1000 g ⎞ Unit Cost = ⎜ ⎟ ⎜ ⎟ = \$8.75/kg ⎜ ⎟ ⎜ ⎟ ⎝ 320 g ⎠ ⎝ 1 kg ⎠ Therefore, the steak at the international market is a better buy. PROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.

1-10 1-34E The thrust developed by the jet engine of a Boeing 777 is given to be 85,000 pounds. This thrust is to be expressed in N and kgf. Analysis Noting that 1 lbf = 4.448 N and 1 kgf = 9.81 N, the thrust developed can be expressed in two other units as ⎛ 4.448 N ⎞ 5 Thrust in N: Thrust = (85,000 lbf )⎜ ⎟ = 3.78×10 N ⎝ 1 lbf ⎠ 5 ⎛ 1 kgf ⎞ 4 Thrust in kgf: Thrust = (37.8×10 N)⎜ ⎟ = 3.85×10 kgf ⎝ 9.81 N ⎠ 1-35 Design and Essay Problems KJ P ROPRIETARY MATERIAL. © 2008 The McGraw-Hill Companies, Inc. Limited distribution permitted only to teachers and educators for course preparation. If you are a student using this Manual, you are using it without permission.
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