EBK THERMODYNAMICS: AN ENGINEERING APPR
EBK THERMODYNAMICS: AN ENGINEERING APPR
8th Edition
ISBN: 9780100257054
Author: CENGEL
Publisher: YUZU
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Chapter 9.12, Problem 64P

An air-standard cycle, called the dual cycle, with constant specific heats is executed in a closed piston– cylinder system and is composed of the following five processes:

1-2 Isentropic compression with a compression ratio, r = V1/V2

2-3 Constant-volume heat addition with a pressure ratio, rp = P3/P2

3-4 Constant-pressure heat addition with a volume ratio, rc V4/V3

4-5 Isentropic expansion while work is done until V5 = V1

5-1 Constant-volume heat rejection to the initial state

  1. (a)   Sketch the P-ν and T-s diagrams for this cycle.
  2. (b)   Obtain an expression for the cycle thermal efficiency as a function of k, r, rc, and rp.
  3. (c)   Evaluate the limit of the efficiency as rp approaches unity, and compare your answer with the expression for the Diesel cycle efficiency.
  4. (d)   Evaluate the limit of the efficiency as rc approaches unity, and compare your answer with the expression for the Otto cycle efficiency.

(a)

Expert Solution
Check Mark
To determine

Draw the Pv and Ts diagrams for the given cycle.

Answer to Problem 64P

The Pv and Ts diagrams for the given cycle are shown as in Figure (1).

Explanation of Solution

Draw the Pv and Ts diagram for the given cycle.

EBK THERMODYNAMICS: AN ENGINEERING APPR, Chapter 9.12, Problem 64P

Thus, the Pv and Ts diagrams for the given cycle are shown as in Figure (1)

(b)

Expert Solution
Check Mark
To determine

The expression for the back work ratio as a function of k and r.

Answer to Problem 64P

The expression for the back work ratio as a function of k,r,rc,andrp is 1rckrp1rk1(rp1)+krprk1(rc1)_.

Explanation of Solution

Apply first law to the closed system for processes 2-3, 3-4, and 5-1 to get the expression of qinandqout.

qin=cv(T3T2)+cp(T4T3)

qout=cv(T5T1)

Here, heat added to the system and heat rejected from the system is qinandqout, constant volume specific heat is cv, temperature at state 1, 2, 3, 4, and 5 are T1,T2,T3,T4,andT5, and constant pressure specific heat is cp.

Express the cycle thermal efficiency.

ηth=1qoutqin (I)

Conclusion:

Process 1-2: Isentropic

Calculate the ratio of T2/T1.

T2T1=(v1v2)k1=rk1

Here, volume at states 1 and 2 is v1,v2, compression ratio is r, and specific heat ratio is k.

Process 2-3: Constant volume

Calculate the expression for T3/T2.

T3T2=P3v3P2v2T3T2=P3P2=rp

Here, pressure at state 1 and 2 is P1andP2, and pressure ratio is rp

Process 3-4: Constant pressure

Calculate the expression for T4/T3.

P4v4T4=P3v3T3T4T3=v4v3T4T3=rc

Here, compression ratio is rc.

Process 4-5: Isentropic

Calculate the expression for T5/T4.

T5T4=(v4v5)k1T5T4=(v4v1)k1T5T4=(rcv3v1)k1T5T4=(rcv2v1)k1

T5T4=(rcr)k1

Process 5-1: Constant volume

Calculate the expression for T5/T1.

T5T1=T5T4T4T3T3T2T2T1

Substitute (rcr)k1 for T5T4, rc for T4T3, rp for T3T2, and rk1 for T2T1.

T5T1=(rcr)k1(rc)rp(rk1)=rckrp

Calculate the ratio of T3/T1.

T3T1=T3T2T2T1

Substitute rp for T3T2 and rk1 for T2T1.

T3T1=rprk1

Substitute cv(T3T2)+cp(T4T3) for qin and cv(T5T1) for qout in equation (I).

ηth=1cv(T5T1)cv(T3T2)+cp(T4T3)=1T1(T5/T11)T2(T3/T21)+kT3T1(T4/T31)=1(T5/T11)T2T1(T3/T21)+kT3T1(T4/T31) (II)

Substitute rprk1 for T3/T1, rp for T3T2, rc for T4T3, rk1 for T2T1, and rckrp for T5T1 in Equation (II).

ηth=1(rckrp1)rk1(rp1)+krprk1(rc1)

Thus, the expression for the back work ratio as a function of k,r,rc,andrp is 1rckrp1rk1(rp1)+krprk1(rc1)_.

(c)

Expert Solution
Check Mark
To determine

The limit of the efficiency as rp approaches unity.

Answer to Problem 64P

The limit of the efficiency as rp approaches unity is 11rk1[rck1k(rc1)].

Explanation of Solution

Recall the expression for the back work ratio as a function of k,r,rc,andrp and apply the limit as rp approaches unity.

limrp1ηth=1{limrp1rckrp1rk1(rp1)+krprk1(rc1)}=11rk1[rck1k(rc1)]

Thus, the limit of the efficiency as rp approaches unity is 11rk1[rck1k(rc1)].

The limit of the efficiency as rp approaches unity is same as the thermal efficiency of diesel cycle.

(d)

Expert Solution
Check Mark
To determine

The limit of the efficiency as rc approaches unity.

Answer to Problem 64P

The limit of the efficiency as rc approaches unity is 11rk1.

Explanation of Solution

Recall the expression for the back work ratio as a function of k,r,rc,andrp and apply the limit as rc approaches unity.

limrp1ηth=1{limrp1rckrp1rk1(rp1)+krprk1(rc1)}=1[rp1rk1(rp1)]=11rk1

Thus, the limit of the efficiency as rc approaches unity is 11rk1.

The limit of the efficiency as rc approaches unity is same as the thermal efficiency of Otto cycle.

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Chapter 9 Solutions

EBK THERMODYNAMICS: AN ENGINEERING APPR

Ch. 9.12 - Prob. 11PCh. 9.12 - Prob. 12PCh. 9.12 - Prob. 13PCh. 9.12 - Prob. 15PCh. 9.12 - Prob. 16PCh. 9.12 - Prob. 17PCh. 9.12 - Prob. 18PCh. 9.12 - Repeat Prob. 919 using helium as the working...Ch. 9.12 - Consider a Carnot cycle executed in a closed...Ch. 9.12 - Prob. 21PCh. 9.12 - Prob. 22PCh. 9.12 - What four processes make up the ideal Otto cycle?Ch. 9.12 - Are the processes that make up the Otto cycle...Ch. 9.12 - How do the efficiencies of the ideal Otto cycle...Ch. 9.12 - How does the thermal efficiency of an ideal Otto...Ch. 9.12 - Prob. 27PCh. 9.12 - Why are high compression ratios not used in...Ch. 9.12 - An ideal Otto cycle with a specified compression...Ch. 9.12 - Prob. 30PCh. 9.12 - Prob. 31PCh. 9.12 - Prob. 32PCh. 9.12 - An ideal Otto cycle has a compression ratio of 8....Ch. 9.12 - Prob. 35PCh. 9.12 - Prob. 36PCh. 9.12 - Prob. 37PCh. 9.12 - An ideal Otto cycle with air as the working fluid...Ch. 9.12 - Repeat Prob. 940E using argon as the working...Ch. 9.12 - Prob. 40PCh. 9.12 - Prob. 41PCh. 9.12 - Prob. 42PCh. 9.12 - Prob. 43PCh. 9.12 - Prob. 44PCh. 9.12 - Prob. 45PCh. 9.12 - Prob. 46PCh. 9.12 - Prob. 47PCh. 9.12 - Prob. 48PCh. 9.12 - Prob. 49PCh. 9.12 - Prob. 50PCh. 9.12 - Prob. 51PCh. 9.12 - Prob. 52PCh. 9.12 - Prob. 53PCh. 9.12 - Prob. 54PCh. 9.12 - Repeat Prob. 957, but replace the isentropic...Ch. 9.12 - Prob. 57PCh. 9.12 - Prob. 58PCh. 9.12 - Prob. 59PCh. 9.12 - The compression ratio of an ideal dual cycle is...Ch. 9.12 - Repeat Prob. 962 using constant specific heats at...Ch. 9.12 - Prob. 63PCh. 9.12 - An air-standard cycle, called the dual cycle, with...Ch. 9.12 - Prob. 65PCh. 9.12 - Prob. 66PCh. 9.12 - Consider the ideal Otto, Stirling, and Carnot...Ch. 9.12 - Consider the ideal Diesel, Ericsson, and Carnot...Ch. 9.12 - An ideal Ericsson engine using helium as the...Ch. 9.12 - An ideal Stirling engine using helium as the...Ch. 9.12 - Prob. 71PCh. 9.12 - Prob. 72PCh. 9.12 - Prob. 73PCh. 9.12 - Prob. 74PCh. 9.12 - Prob. 75PCh. 9.12 - For fixed maximum and minimum temperatures, what...Ch. 9.12 - What is the back work ratio? What are typical back...Ch. 9.12 - Why are the back work ratios relatively high in...Ch. 9.12 - How do the inefficiencies of the turbine and the...Ch. 9.12 - A simple ideal Brayton cycle with air as the...Ch. 9.12 - A gas-turbine power plant operates on the simple...Ch. 9.12 - Prob. 82PCh. 9.12 - Prob. 83PCh. 9.12 - Prob. 85PCh. 9.12 - 9–86 Consider a simple Brayton cycle using air as...Ch. 9.12 - 9–87 Air is used as the working fluid in a simple...Ch. 9.12 - Air is used as the working fluid in a simple ideal...Ch. 9.12 - An aircraft engine operates on a simple ideal...Ch. 9.12 - 9–91E A gas-turbine power plant operates on a...Ch. 9.12 - Prob. 92PCh. 9.12 - 9–93 A gas-turbine power plant operates on the...Ch. 9.12 - A gas-turbine power plant operates on a modified...Ch. 9.12 - Prob. 95PCh. 9.12 - Prob. 96PCh. 9.12 - Prob. 97PCh. 9.12 - Prob. 98PCh. 9.12 - 9–99 A gas turbine for an automobile is designed...Ch. 9.12 - Prob. 100PCh. 9.12 - A gas-turbine engine operates on the ideal Brayton...Ch. 9.12 - An ideal regenerator (T3 = T5) is added to a...Ch. 9.12 - Prob. 103PCh. 9.12 - Prob. 104PCh. 9.12 - Prob. 106PCh. 9.12 - A Brayton cycle with regeneration using air as the...Ch. 9.12 - Prob. 108PCh. 9.12 - Prob. 109PCh. 9.12 - Prob. 110PCh. 9.12 - Prob. 111PCh. 9.12 - Prob. 112PCh. 9.12 - Prob. 113PCh. 9.12 - Prob. 114PCh. 9.12 - Prob. 115PCh. 9.12 - A simple ideal Brayton cycle without regeneration...Ch. 9.12 - A simple ideal Brayton cycle is modified to...Ch. 9.12 - Prob. 118PCh. 9.12 - Consider a regenerative gas-turbine power plant...Ch. 9.12 - Repeat Prob. 9123 using argon as the working...Ch. 9.12 - Consider an ideal gas-turbine cycle with two...Ch. 9.12 - Repeat Prob. 9125, assuming an efficiency of 86...Ch. 9.12 - Prob. 123PCh. 9.12 - Prob. 124PCh. 9.12 - Prob. 126PCh. 9.12 - Prob. 127PCh. 9.12 - Prob. 128PCh. 9.12 - Prob. 129PCh. 9.12 - A turbojet is flying with a velocity of 900 ft/s...Ch. 9.12 - Prob. 131PCh. 9.12 - A pure jet engine propels an aircraft at 240 m/s...Ch. 9.12 - A turbojet aircraft is flying with a velocity of...Ch. 9.12 - Prob. 134PCh. 9.12 - Consider an aircraft powered by a turbojet engine...Ch. 9.12 - 9–137 Air at 7°C enters a turbojet engine at a...Ch. 9.12 - Prob. 138PCh. 9.12 - Prob. 139PCh. 9.12 - 9–140E Determine the exergy destruction associated...Ch. 9.12 - Prob. 141PCh. 9.12 - Prob. 142PCh. 9.12 - Prob. 143PCh. 9.12 - Prob. 144PCh. 9.12 - Prob. 146PCh. 9.12 - A gas-turbine power plant operates on the...Ch. 9.12 - Prob. 149PCh. 9.12 - Prob. 150RPCh. 9.12 - Prob. 151RPCh. 9.12 - Prob. 152RPCh. 9.12 - Prob. 153RPCh. 9.12 - Prob. 154RPCh. 9.12 - Prob. 155RPCh. 9.12 - Prob. 156RPCh. 9.12 - Prob. 157RPCh. 9.12 - Prob. 159RPCh. 9.12 - Prob. 161RPCh. 9.12 - Prob. 162RPCh. 9.12 - Prob. 163RPCh. 9.12 - Consider a simple ideal Brayton cycle with air as...Ch. 9.12 - Prob. 165RPCh. 9.12 - Helium is used as the working fluid in a Brayton...Ch. 9.12 - Consider an ideal gas-turbine cycle with one stage...Ch. 9.12 - Prob. 169RPCh. 9.12 - Prob. 170RPCh. 9.12 - Prob. 173RPCh. 9.12 - Prob. 174RPCh. 9.12 - Prob. 184FEPCh. 9.12 - For specified limits for the maximum and minimum...Ch. 9.12 - Prob. 186FEPCh. 9.12 - Prob. 187FEPCh. 9.12 - Helium gas in an ideal Otto cycle is compressed...Ch. 9.12 - Prob. 189FEPCh. 9.12 - Prob. 190FEPCh. 9.12 - Consider an ideal Brayton cycle executed between...Ch. 9.12 - An ideal Brayton cycle has a net work output of...Ch. 9.12 - In an ideal Brayton cycle, air is compressed from...Ch. 9.12 - In an ideal Brayton cycle with regeneration, argon...Ch. 9.12 - In an ideal Brayton cycle with regeneration, air...Ch. 9.12 - Consider a gas turbine that has a pressure ratio...Ch. 9.12 - An ideal gas turbine cycle with many stages of...Ch. 9.12 - Prob. 198FEP
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