A.5
B.7
C.12
D.20
E.24
Related Mcqs:
- The range of compression ratio in a gas turbine is
- During idling in a compression ignition engine the air fuel ratio may be of the order of
- Compression ratio in case of gas engines waries in the range
- Two SI engines run at same speed and develop same power but have different compression ratio. The engine with higher compression ratio will have its ignition advance
- A gas turbine cycle operates through pressures ratio of 5. Air enters the compressor at atmospheric pressure and 25?C and entry to the turbine is at 800?C. The thermal efficiency of the plant has been found to be 37%. Now, if compressor and turbine efficiencies of 80% are taken into account, the value, of thermal efficiency will be
- Highest useful compression ratio is the compression ratio at which
- The mean effective pressure of a diesel cycle having fixed compression ratio will increase if cut off ratio will
- With increase in pressure ratio, thermal efficiency of a simple gas turbine plant with fixed turbine inlet temperature
- The thermal efficiency of a dual cycle engine with fixed compression ratio and fixed quantity of het and with increase in pressure ratio, will
- The maximum temperature in a gas turbine is of the order of
