The weight per horse power ratio for gas in Turbine as compared to I.C. engine and steam turbine is

A. Same

B. Higher

C. Lower

D. None of these

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  1. 1 m of air at atmospheric condition weighs approximately
  2. The thrust of a jet propulsion power unit can be increased by
  3. The reason for volumetric efficiency of reciprocating compressor being less than 100 percent is
  4. Cylinder clearance in a compressor should be
  5. Gas turbines for power generation are normally used
  6. For perfect intercooling in a three stage compressor
  7. Pick up the correct statement
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  10. The thermal efficiency of a simple gas turbine for a given turbine inlet temperature with increase in…
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  13. The thermodynamic efficiency of rotary compressor is based on
  14. The compressor capacity with decrease in suction temperature
  15. The work ratio of a gas turbine plant is defined as the ratio of
  16. Ratio of compression is the ratio of
  17. When air is to be compressed at a high pressure, then it is advantageous to use
  18. In a single stage, single acting reciprocating air compressor without clearance volume, the workdone…
  19. In jet propulsion power unit, the inlet duct of diverging shape is used in order to
  20. In multistage compressor, the isothermal compression is achieved by
  21. The volume of air delivered in a medium capacity air compressor per unit time is
  22. A rocket engine uses ________ for the combustion of its fuel.
  23. The pressure ratio in gas turbines is of the order of
  24. It is not possible to use closed gas turbine cycle in aeronautical engines because
  25. Turbofan engine employs
  26. The fuel consumption in gas turbines is accounted for by
  27. For perfect intercooling in a two stage compressor
  28. A 3 m³/min compressor means that it
  29. The material commonly used for air craft gas turbine is
  30. Inter-cooling in gas turbine results in