A. increase temperature
B. reduce turbine size
C. increase power output
D. increase speed
E. increase pressure ratio
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Related Mcqs:
- Reheating in gas turbine results in___________________?
- A. increase of work ratio B. decrease of thermal efficiency C. decrease of work ratio D. both A. and B. above E. both B. and C. above...
- Reheating in multistage expansion gas turbine results in____________________?
- A. high thermal efficiency B. reduction in compressor work C. decrease of heat loss in exhaust D. maximum work output E. none of the above...
- The pressure ratio for an open cycle gas turbine compared to closed cycle gas turbine of same h.p. is_______________?
- A. low B. high C. same D. low/high depending on make and type E. unpredictable...
- The thermal efficiency of a simple gas turbine for a given turbine inlet temperature with increase in pressure ratio_____________________?
- A. increases B. decreases C. first increases and then decreases D. first decreases and then increases E. remains same...
- There is a certain pressure ratio (optimum) for a gas turbine at which its thermal efficiency is maximum. With increase in turbine temperature, the value of pressure ratio for the peak efficiency would__________________?
- A. remain same B. decrease C. increase D. unpredictable E. none of the above...
- As the turbine inlet temperature increases, the thermal efficiency of gas turbine for the optimum pressure ratio_____________________?
- A. increases B. decreases C. remains same D. first increases and then decreases E. first decreases and then increases...
- If infinite number of heaters be used in a gas turbine, then expansion process in turbine approaches _________________?
- A. isothermal B. isentropic C. adiabatic D. isochoric E. isobaric...
- The weight per horse power ratio for gas. turbine as compared to I.C. engine and steam turbine is________________?
- A. same B. higher C. lower D. uncomparable E. unpredictable...
- Maximum temprature in a gas turbine is of the order of COMPRESSORS, GAS TURBINES AND JET ENGINES______________________?
- A. 2500°C B. 2000°C C. 1500°C D. 1000°C E. 700°C...
- The work ratio of simple gas turbine cycle depends on_________________?
- A. pressure ratio B. maximum cycle temperature C. minimum cycle temperature D. all of the above E. none of die above...
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