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A closed gas turbine in which fuel is burnt directly in the air is not possible because of

A. Paucity of O2

B. Increasing gas temperature

C. High specific volume

D. High friction losses

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

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  1. The compressor capacity with decrease in suction temperature
  2. The stagnation pressure rise in a centrifugal compressor takes place
  3. A compressor at high altitudes will require ________ power.
  4. Maximum work is done in compressing air when the compression is
  5. Losses in a centrifugal compressor are due to
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  10. Which of the following statement is correct?
  11. Pick up the wrong statement
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  17. An air compressor may be controlled by
  18. Open cycle gas turbine works on
  19. Volumetric efficiency of air compressors is of the order of
  20. The compression ratio in a gas turbine is of the order of
  21. Pick up the wrong statement about advantages of multistage compression
  22. The output of a gas turbine is 300 KW and its efficiency is 20 percent, the heat supplied is
  23. In jet engines the products of combustion after passing through the gas turbine are discharged into
  24. A gas turbine used in air craft should have
  25. After-cooler is used to
  26. In an axial flow compressor, the ratio of pressure in the rotor blades to the pressure rise in the compressor…
  27. A 3 m³/min compressor means that it
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  29. The area of actual indicator diagram on an air compressor as compared to area of ideal indicator diagram…
  30. Standard air is the air at