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Gas turbine works on

A. Brayton or Atkinson cycle

B. Carnot cycle

C. Rankine cycle

D. Erricson cycle

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  1. A machine used to raise the pressure of air is called
  2. The ratio of the net work obtained from the gas turbine plant to the turbine work is known as
  3. The closed cycle in gas turbines
  4. Which of the following statement is wrong?
  5. Volumetric efficiency of a compressor decreases with ________ in compression ratio.
  6. The work done per unit mass of air in compression will be least when n is equal to
  7. The fuel consumption in gas turbines is accounted for by
  8. The compression ratio in a gas turbine is of the order of
  9. The compressor efficiency is the
  10. The reason for volumetric efficiency of reciprocating compressor being less than 100 percent is
  11. Ramjet engine
  12. As the turbine inlet temperature increases, the thermal efficiency of gas turbine for the optimum pressure…
  13. Open cycle gas turbine works on
  14. The ratio of outlet whirl velocity to blade velocity in case of centrifugal compressor is called
  15. Which of the following statement is correct as regard to centrifugal compressors?
  16. Which is false statement about multistage compression?
  17. Which of the following statement is correct?
  18. The type of rotary compressor used in aeroplanes, is of
  19. Air-fuel ratio in a jet engine will be of the order of
  20. In a double acting compressor, the air is compressed
  21. The overall isothermal efficiency of compressor is defined as the ratio of
  22. The air entry velocity m a rocket as compared to aircraft is
  23. The compressed air may be used
  24. In open cycle turbojet engines used in military aircraft, reheating the exhaust gas from the turbine…
  25. Isothermal compression though most efficient, but is not practicable because
  26. Separators are generally used in air compressor installations
  27. When the temperature of air leaving the intercooler, in a two stage compression with intercooler, is…
  28. Gas turbine works on
  29. Isothermal compression efficiency, even when running at high speed, can be approached by using
  30. The thrust of a jet propulsion power unit can be increased by