1 Introduction And Basic Concepts 2 Energy, Energy Transfer, And General Energy Analysis 3 Properties Of Pure Substances 4 Energy Analysis Of Closed Systems 5 The Second Law Of Thermodynamics 6 The Second Law Of Thermodynamics 7 Entropy 8 Exergy 9 Gas Power Cycles 10 Vapor And Combined Power Cycles 11 Refrigeration Cycles 12 Thermodynamic Property Relations 13 Gas Mixtures 14 Gascfvapor Mixtures And Air-conditioning 15 Chemical Reactions 16 Chemical And Phase Equilibrium 17 Compressible Flow expand_more
9.1 Basic Considerations In The Analysis Of Power Cycles 9.2 The Carnot Cycle And Its Value In Engineering 9.3 Air-standard Assumptions 9.4 An Overview Of Reciprocating Engines 9.5 Otto Cycle: The Ideal Cycle For Spark-ignition Engines 9.6 Diesel Cycle: The Ideal Cycle For Compression-ignition Engines 9.7 Stirling And Ericsson Cycles 9.8 Brayton Cycle: The Ideal Cycle For Gas-turbine Engines 9.9 The Brayton Cycle With Regeneration 9.10 The Brayton Cycle With Lntercooling, Reheating, And Regeneration 9.11 Ideal Jet-propulsion Cycles 9.12 Second-law Analysis Of Gas Power Cycles expand_more
Problem 1P: What are the air-standard assumptions? Problem 2P: What is the difference between air-standard assumptions and the cold-air-standard assumptions? Problem 3P Problem 4P: How does the thermal efficiency of an ideal cycle, in general, compare to that of a Carnot cycle... Problem 5P: How are the combustion and exhaust processes modeled under the air-standard assumptions? Problem 6P: What does the area enclosed by the cycle represent on a P-v diagram? How about on a T-s diagram? Problem 7P Problem 8P: Can the mean effective pressure of an automobile engine in operation be less than the atmospheric... Problem 9P: What is the difference between spark-ignition and compression-ignition engines? Problem 10P Problem 11P Problem 12P: Can any ideal gas power cycle have a thermal efficiency greater than 55 percent when using thermal... Problem 13P Problem 14P Problem 15P Problem 16P Problem 17P Problem 18P Problem 19P Problem 20P: Repeat Prob. 919 using helium as the working fluid. Problem 21P: The thermal energy reservoirs of an ideal gas Carnot cycle are at 1240F and 40F, and the device... Problem 22P: Consider a Carnot cycle executed in a closed system with 0.6 kg of air. The temperature limits of... Problem 23P: Consider a Carnot cycle executed in a closed system with air as the working fluid. The maximum... Problem 24P: What four processes make up the ideal Otto cycle? Problem 25P: Are the processes that make up the Otto cycle analyzed as closed-system or steady-flow processes?... Problem 26P: How do the efficiencies of the ideal Otto cycle and the Carnot cycle compare for the same... Problem 27P: How does the thermal efficiency of an ideal Otto cycle change with the compression ratio of the... Problem 28P: Why are high compression ratios not used in spark-ignition engines? Problem 29P: An ideal Otto cycle with a specified compression ratio is executed using (a) air, (b) argon, and (c)... Problem 30P Problem 31P Problem 32P: Determine the mean effective pressure of an ideal Otto cycle that uses air as the working fluid; its... Problem 33P: Reconsider Prob. 932E. Determine the rate of heat addition and rejection for this ideal Otto cycle... Problem 34P: An ideal Otto cycle has a compression ratio of 8. At the beginning of the compression process, air... Problem 36P Problem 37P: A spark-ignition engine has a compression ratio of 10, an isentropic compression efficiency of 85... Problem 38P: An ideal Otto cycle has a compression ratio of 7. At the beginning of the compression process, P1 =... Problem 39P Problem 40P: An ideal Otto cycle with air as the working fluid has a compression ratio of 8. The minimum and... Problem 41P: Repeat Prob. 940E using argon as the working fluid. Problem 42P: Someone has suggested that the air-standard Otto cycle is more accurate if the two isentropic... Problem 43P: Repeat Prob. 942 when isentropic processes are used in place of the polytropic processes? Problem 44P Problem 45P Problem 46P Problem 47P Problem 48P Problem 49P Problem 50P Problem 51P Problem 52P Problem 53P Problem 54P Problem 55P Problem 56P Problem 57P Problem 58P: Repeat Prob. 957, but replace the isentropic expansion process with a polytropic expansion process... Problem 60P Problem 61P Problem 62P: The compression ratio of an ideal dual cycle is 14. Air is at 100 kPa and 300 K at the beginning of... Problem 64P: Repeat Prob. 962 using constant specific heats at room temperature. Is the constant specific heat... Problem 65P Problem 66P Problem 67P Problem 68P: An air-standard cycle, called the dual cycle, with constant specific heats is executed in a closed... Problem 69P Problem 70P Problem 71P: Consider the ideal Otto, Stirling, and Carnot cycles operating between the same temperature limits.... Problem 72P: Consider the ideal Diesel, Ericsson, and Carnot cycles operating between the same temperature... Problem 73P: An ideal Ericsson engine using helium as the working fluid operates between temperature limits of... Problem 74P: An ideal Stirling engine using helium as the working fluid operates between temperature limits of... Problem 75P Problem 76P Problem 77P Problem 78P Problem 79P Problem 80P: For fixed maximum and minimum temperatures, what is the effect of the pressure ratio on (a) the... Problem 81P: What is the back work ratio? What are typical back work ratio values for gas-turbine engines? Problem 82P: Why are the back work ratios relatively high in gas-turbine engines? Problem 83P: How do the inefficiencies of the turbine and the compressor affect (a) the back work ratio and (b)... Problem 84P: A simple ideal Brayton cycle with air as the working fluid has a pressure ratio of 10. The air... Problem 85P: A stationary gas-turbine power plant operates on a simple ideal Brayton cycle with air as the... Problem 86P: A gas-turbine power plant operates on the simple Brayton cycle with air as the working fluid and... Problem 87P Problem 88P Problem 89P: Repeat Prob. 988 when the isentropic efficiency of the turbine is 90 percent. Problem 90P: Repeat Prob. 988 when the isentropic efficiency of the turbine is 90 percent and that of the... Problem 91P: Repeat Prob. 988 when the isentropic efficiencies of the turbine and compressor are 90 percent and... Problem 92P: Air is used as the working fluid in a simple ideal Brayton cycle that has a pressure ratio of 12, a... Problem 93P: An aircraft engine operates on a simple ideal Brayton cycle with a pressure ratio of 10. Heat is... Problem 94P: Repeat Prob. 993 for a pressure ratio of 15. Problem 95P: A gas-turbine power plant operates on the simple Brayton cycle between the pressure limits of 100... Problem 96P: A simple ideal Brayton cycle uses argon as the working fluid. At the beginning of the compression,... Problem 97P: A gas-turbine power plant operates on a modified Brayton cycle shown in the figure with an overall... Problem 98P: A gas-turbine power plant operating on the simple Brayton cycle has a pressure ratio of 7. Air... Problem 99P Problem 100P Problem 101P Problem 102P Problem 103P Problem 104P Problem 105P: A gas turbine for an automobile is designed with a regenerator. Air enters the compressor of this... Problem 106P: Rework Prob. 9105 when the compressor isentropic efficiency is 87 percent and the turbine isentropic... Problem 107P: A gas-turbine engine operates on the ideal Brayton cycle with regeneration, as shown in Fig. P9105.... Problem 108P: An ideal regenerator (T3 = T5) is added to a simple ideal Brayton cycle (see Fig. P9105). Air enters... Problem 109P Problem 111P Problem 112P: A Brayton cycle with regeneration using air as the working fluid has a pressure ratio of 7. The... Problem 113P Problem 114P Problem 115P Problem 116P Problem 117P Problem 118P Problem 119P Problem 120P Problem 121P: A simple ideal Brayton cycle without regeneration is modified to incorporate multistage compression... Problem 122P: A simple ideal Brayton cycle is modified to incorporate multistage compression with intercooling,... Problem 123P: Consider a regenerative gas-turbine power plant with two stages of compression and two stages of... Problem 124P: Repeat Prob. 9123 using argon as the working fluid. Problem 125P: Consider an ideal gas-turbine cycle with two stages of compression and two stages of expansion. The... Problem 126P: Repeat Prob. 9125, assuming an efficiency of 86 percent for each compressor stage and an efficiency... Problem 127P: A gas turbine operates with a regenerator and two stages of reheating and intercooling. Air enters... Problem 128P Problem 129P Problem 130P Problem 131P Problem 132P: Air at 7C enters a turbojet engine at a rate of 16 kg/s and at a velocity of 220 m/s (relative to... Problem 133P Problem 134P: A turbojet is flying with a velocity of 900 ft/s at an altitude of 20,000 ft, where the ambient... Problem 135P: A pure jet engine propels an aircraft at 240 m/s through air at 45 kPa and 13C. The inlet diameter... Problem 136P: A turbojet aircraft is flying with a velocity of 280 m/s at an altitude of 9150 m, where the ambient... Problem 137P Problem 138P Problem 139P: Reconsider Prob. 9138E. How much change would result in the thrust if the propeller diameter were... Problem 140P: Consider an aircraft powered by a turbojet engine that has a pressure ratio of 9. The aircraft is... Problem 142P: An ideal Otto cycle has a compression ratio of 8. At the beginning of the compression process, air... Problem 143P: An air-standard Diesel cycle has a compression ratio of 16 and a cutoff ratio of 2. At the beginning... Problem 144P Problem 145P Problem 146P Problem 147P Problem 148P: A Brayton cycle with regeneration using air as the working fluid has a pressure ratio of 7. The... Problem 150P Problem 151P: A gas turbine operates with a regenerator and two stages of reheating and intercooling. Air enters... Problem 152P: A gas-turbine power plant operates on the regenerative Brayton cycle between the pressure limits of... Problem 153P Problem 154RP: An air-standard cycle with variable specific heats is executed in a closed system with 0.003 kg of... Problem 155RP Problem 156RP Problem 157RP Problem 158RP Problem 159RP Problem 160RP Problem 161RP Problem 162RP: Consider an engine operating on the ideal Diesel cycle with air as the working fluid. The volume of... Problem 163RP: Repeat Prob. 9162 using argon as the working fluid. Problem 164RP Problem 165RP Problem 166RP Problem 167RP Problem 168RP: Consider an ideal Stirling cycle using air as the working fluid. Air is at 400 K and 200 kPa at the... Problem 169RP Problem 170RP: Consider a simple ideal Brayton cycle with air as the working fluid. The pressure ratio of the cycle... Problem 171RP Problem 172RP: A Brayton cycle with a pressure ratio of 15 operates with air entering the compressor at 70 kPa and... Problem 173RP: Helium is used as the working fluid in a Brayton cycle with regeneration. The pressure ratio of the... Problem 174RP: Consider an ideal gas-turbine cycle with one stage of compression and two stages of expansion and... Problem 176RP Problem 177RP Problem 180RP Problem 181RP Problem 182RP Problem 192FEP: For specified limits for the maximum and minimum temperatures, the ideal cycle with the lowest... Problem 193FEP: A Carnot cycle operates between the temperature limits of 300 and 2000 K and produces 400 kW of net... Problem 194FEP Problem 195FEP Problem 196FEP: Helium gas in an ideal Otto cycle is compressed from 20C and 2.5 to 0.25 L, and its temperature... Problem 197FEP Problem 198FEP Problem 199FEP: In an ideal Brayton cycle, air is compressed from 95 kPa and 25C to 1400 kPa. Under... Problem 200FEP: In an ideal Brayton cycle, air is compressed from 100 kPa and 25C to 1 MPa, and then heated to 927C... Problem 201FEP: Consider an ideal Brayton cycle executed between the pressure limits of 1200 and 100 kPa and... Problem 202FEP: An ideal Brayton cycle has a net work output of 150 kJ/kg and a back work ratio of 0.4. If both the... Problem 203FEP: In an ideal Brayton cycle with regeneration, argon gas is compressed from 100 kPa and 25C to 400... Problem 204FEP: In an ideal Brayton cycle with regeneration, air is compressed from 80 kPa and 10C to 400 kPa and... Problem 205FEP: Consider a gas turbine that has a pressure ratio of 6 and operates on the Brayton cycle with... Problem 206FEP: An ideal gas turbine cycle with many stages of compression and expansion and a regenerator of 100... format_list_bulleted