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When the temperature of air leaving the intercooler, in a two stage compression with intercooler, is ________ the original atmospheric air temperature, then the intercooling is known as perfect or complete intercooling.

A. Equal to

B. Less than

C. More than

D. None of these

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  1. Compression efficiency is compared against
  2. Water is injected in gas turbine cycle to
  3. Ram compression in turbojet involves
  4. Gas turbine works on
  5. The pressure ratio for an open cycle gas turbine compared to closed cycle gas turbine of same h.p. is
  6. The ratio of the indicated power to the shaft power or brake power of the motor or engine required to…
  7. The thrust of a jet propulsion power unit can be increased by
  8. Separators in compressor installations are located
  9. Which is false statement about air receivers?
  10. The volumetric efficiency of compressor with increase in compression ratio will
  11. The fuel consumption in gas turbines is accounted for by
  12. An ideal air compressor cycle with clearance on PV diagram can be represented by following processes
  13. The ratio of isentropic work to Euler work is known as
  14. Volumetric efficiency of air compressors is of the order of
  15. The degree of reaction is usually kept ________ for all types of axial flow compressors.
  16. Mechanical efficiency of gas turbines as compared to I.C engines is
  17. The ratio of the net work obtained from the gas turbine plant to the turbine work is known as
  18. If p₁ is the pressure of air entering the L.P, cylinder and p₃ is the pressure of air…
  19. With the decrease in compression ratio, the volumetric efficiency
  20. The efficiency of jet engine is
  21. Which of the following plants is smallest and lightest for generating a given amount of power?
  22. A compressor mostly used for supercharging of I.C. engines is
  23. Temperature of gases at end of compression as compared to exhaust gases in a gas turbine is
  24. The performance of air compressor at high altitudes will be ________ as compared to that at sea level.
  25. Isothermal compression though most efficient, but is not practicable because
  26. The specific output per kg mass flow rate of a gas turbine (having fixed efficiencies of compressor…
  27. Phenomenon of choking in compressor means
  28. Ratio of indicated H.P. and brake H.P. is known as
  29. Work ratio of a gas turbine plant is ratio of
  30. The maximum propulsion efficiency of a turbojet is attained at around following speed