The working fluid in a turbine is

A. In two phases

B. In three phases

C. In a single phase

D. In the form of air and water mixture

Please do not use chat terms. Example: avoid using "grt" instead of "great".

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  1. The ratio of the discharge pressure to the inlet pressure of air is called
  2. The performance of air compressor at high altitudes will be ________ as compared to that at sea level.
  3. Rotary compressor is best suited for
  4. Work ratio of a gas turbine plant is ratio of
  5. If the flow of air through the compressor is perpendicular to its axis, then it is a
  6. The compressor capacity with decrease in suction temperature
  7. A closed gas turbine in which fuel is burnt directly in the air is not possible because of
  8. A closed cycle gas turbine works on
  9. Which of the following statement is correct?
  10. Work ratio of a gas turbine may be improved by
  11. Inter-cooling in multistage compressors is done
  12. Axial flow compressor has the following advantage over centrifugal compressor
  13. Maximum work is done in compressing air when the compression is
  14. The volume of air delivered in a medium capacity air compressor per unit time is
  15. Euler's equation can be used for
  16. In jet propulsion power unit, the inlet duct of diverging shape is used in order to
  17. A machine used to raise the pressure of air is called
  18. Volumetric efficiency of air compressors is of the order of
  19. Gas turbine works on
  20. The work done per unit mass of air in compression will be least when n is equal to
  21. Pick up the false statement
  22. The main purpose of reheating in gas turbine is to
  23. In a centrifugal compressor, the ratio of the ________ to the blade velocity is called slip factor.
  24. The axial flow compressor is preferred in aircraft gas turbines because of
  25. Compression efficiency is compared against
  26. In air breathing jet engine, the jet is formed by expanding
  27. In a jet engine, the air-fuel ratio is
  28. The absolute pressure of air at the outlet of a compressor is called
  29. The overall efficiency of the compressed air system is the
  30. In the cross compounding of the gas turbine plant