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The thermal efficiency of a gas turbine as compared to a diesel plant is

A. Same

B. More

C. Less

D. Depends on other factors

Correct Answer : C.


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  1. For perfect intercooling in a two stage compressor
  2. The absolute pressure of air at the outlet of a compressor is called
  3. In air breathing jet engine, the jet is formed by expanding
  4. Efficiency of gas turbine is increased by
  5. 1 m of air at atmospheric condition weighs approximately
  6. Work ratio of a gas turbine may be improved by
  7. The efficiency of a jet engine is higher at
  8. The compressor efficiency is the
  9. The main purpose of reheating in gas turbine is to
  10. Which is false statement about multistage compression?
  11. The most efficient method of compressing air is to compress it
  12. Which of the following statement is correct?
  13. In a compressor, free air delivered is the actual volume delivered at the stated pressure reduced to
  14. For speed above 3000 km/hour, it is more advantageous to use
  15. The pressure ratio for an open cycle gas turbine compared to closed cycle gas turbine of same h.p. is
  16. In air compressors, free air delivery means the
  17. The effective power of gas turbines is increased by adding the following in compressor
  18. The efficiency and work ratio of a gas turbine plant can be increased by
  19. The pressure of air at the beginning of the compression stroke is ________ the atmospheric pressure.
  20. Maximum temperature in a gas turbine is of the order of
  21. A gas turbine used in air craft should have
  22. The pressure and temperature conditions of air at the suction of compressor are
  23. Only rocket engines can be propelled to space because
  24. An air compressor may be controlled by
  25. For minimum work required to compress and deliver a quantity of air by multistage compression
  26. In jet engines, for the efficient production of large power, fuel is burnt in an atmosphere of
  27. The fuel consumption in gas turbines is accounted for by
  28. The ratio of the indicated power to the shaft power or brake power of the motor or engine required to…
  29. Turbofan engine employs
  30. The maximum compression ratio in an actual single stage axial flow compressor is of the order of