A jet engine has

A. No propeller

B. Propeller in front

C. Propeller at back

D. Propeller on the top

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

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  1. Aeroplanes employ following type of compressor
  2. The compressor capacity is defined as the
  3. The criterion of the thermodynamic efficiency for rotary compressor is
  4. For perfect intercooling in a three stage compressor
  5. The air power of the compressor is also known as
  6. Temperature of gases at end of compression as compared to exhaust gases in a gas turbine is
  7. The degree of reaction is usually kept ________ for all types of axial flow compressors.
  8. If p₁, is the pressure of air entering the L.P. cylinder and p₂ is the pressure of air…
  9. Gas turbine works on
  10. For minimum work required to compress and deliver a quantity of air by multistage compression
  11. After-cooler is used to
  12. The compressor capacity with decrease in suction temperature
  13. The maximum temperature in a gas turbine is
  14. A compressor at high altitudes will require ________ power.
  15. Reheating in a multistage expansion gas turbine __________ compressor work.
  16. The degree of reaction of an axial flow turbine is the ratio of isentropic temperature drop in a blade…
  17. Inter cooling in compressors
  18. The pressure and temperature conditions of air at the suction of compressor are
  19. In which case the air-fuel ratio is likely to be maximum?
  20. A gas turbine used in air craft should have
  21. Which of the following statement is correct?
  22. The ratio of the net work obtained from the gas turbine plant to the turbine work is known as
  23. The volumetric efficiency of compressor with increase in compression ratio will
  24. The intercooler pressure, for minimum work required, for a two stage reciprocating air compressor, is…
  25. The absolute pressure of air at the outlet of a compressor is called
  26. The efficiency of a jet engine is higher at
  27. For supplying intermittent small quantity of air at high pressure, following compressor is best suited
  28. In the axial flow gas turbine, the work ratio is the ratio of
  29. The compressor performance at higher altitude compared to sea level will be
  30. Ratio of indicated h.p. to shaft h.p. in known as