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Temperature of gases at end of compression as compared to exhaust gases in a gas turbine is

A. Higher

B. Lower

C. Equal

D. Cant be compared

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  1. Which of the following statement is correct?
  2. The minimum work required for a three stage reciprocating air compressor is ________ the work required…
  3. The propulsive power of the rocket is (where v₁ = Jet velocity, and v₂ = Aircraft velocity)
  4. Ramjet engine
  5. The working fluid in a turbine is
  6. In an axial flow compressor, the ratio of pressure in the rotor blades to the pressure rise in the compressor…
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  12. Efficiency of gas turbine is increased by
  13. In the aircraft propellers
  14. The ratio of isentropic work to Eulers work is known as
  15. The overall isothermal efficiency of the compressor is defined as the ratio of
  16. The net work input required for compressor with increase in clearance volume
  17. Compression efficiency is compared against
  18. The clearance volume of the air compressor is kept minimum because
  19. In a closed cycle gas turbine, the air is compressed
  20. During base load operation, the best method of controlling compressor is
  21. Gas turbine blades are given a rake
  22. If p₁, is the pressure of air entering the L.P. cylinder and p₂ is the pressure of air…
  23. A large clearance volume in a reciprocating compressor results in
  24. An ideal air compressor cycle with clearance on PV diagram can be represented by following processes
  25. Pick up the correct statement
  26. The thrust on the rotor in a centrifugal compressor is produced by
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  28. The work ratio of simple gas turbine cycle depends on
  29. Pressure ratio in gas turbines is the ratio of
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