• recategorized by
728 views
0 0 votes
In a compression ignition engine, the inlet air pressure is $1$ bar and the pressure at the end of isentropic compression is $32.42$ bar. The expansion ratio is $8$. Assuming ratio of specific heats $(γ)$ as $1.4$, the air standard efficiency (in percent) is _______

Please log in or register to answer this question.

Related questions

0 0 votes
0 0 answers
314
314 views
Arjun asked Feb 19, 2017
314 views
A diesel engine has a compression ratio of $17$ and cut-off takes place at $10\%$ of the stroke.Assuming ratio of specific heats $(\gamma)$ as $1.4$, the air-standard eff...
0 0 votes
0 0 answers
301
301 views
Arjun asked Feb 19, 2017
301 views
Which one of the following pairs of equations describes an irreversible heat engine?$\oint \delta Q 0$ and $\oint \dfrac{\delta Q}{T} < 0 \\$$\oint \delta Q< 0$ and $\oin...
0 0 votes
0 0 answers
498
498 views
Arjun asked Feb 9, 2019
498 views
An air standard Otto cycle has thermal efficiency of $0.5$ and the mean effective pressure of the cycle is $1000 \: kPa$. For air, assume specific heat ratio $\gamma=1.4$...
0 0 votes
0 0 answers
340
340 views
Arjun asked Feb 19, 2017
340 views
Steam with specific enthalpy $(h)$ $3214$ $kJ/kg$ enters an adiabatic turbine operating at steady state with a flow rate $10$ $kg/s$. As it expands, at a point where h is...

Related questions

0 0 votes
0 0 answers
314
314 views
Arjun asked Feb 19, 2017
314 views
A diesel engine has a compression ratio of $17$ and cut-off takes place at $10\%$ of the stroke.Assuming ratio of specific heats $(\gamma)$ as $1.4$, the air-standard eff...
0 0 votes
0 0 answers
301
301 views
Arjun asked Feb 19, 2017
301 views
Which one of the following pairs of equations describes an irreversible heat engine?$\oint \delta Q 0$ and $\oint \dfrac{\delta Q}{T} < 0 \\$$\oint \delta Q< 0$ and $\oin...
0 0 votes
0 0 answers
498
498 views
Arjun asked Feb 9, 2019
498 views
An air standard Otto cycle has thermal efficiency of $0.5$ and the mean effective pressure of the cycle is $1000 \: kPa$. For air, assume specific heat ratio $\gamma=1.4$...
0 0 votes
0 0 answers
340
340 views
Arjun asked Feb 19, 2017
340 views
Steam with specific enthalpy $(h)$ $3214$ $kJ/kg$ enters an adiabatic turbine operating at steady state with a flow rate $10$ $kg/s$. As it expands, at a point where h is...
Position:
Show:
Answer:

Add Synced Question

×