Home

For perfect intercooling in a three stage compressor

A. p₂/p₁ = p₃/p₂ = p₄/p₃

B. p₃/p₁ = p₄/p₂

C. p₁ p₂ = p₃ p₄

D. p₁ p₃ = p₂ p₄

Correct Answer : A.


Download Objective type questions of Compressors, Gas Turbines & Jet Engines PDF

Visit our PDF store

Get all objective type questions of Compressors, Gas Turbines & Jet Engines MCQ

Also checkout these categories

Hydraulics & Fluid Machineries MCQ Applied Mechanics and Graphic Statics MCQ Decision Making MCQ Inequalities MCQ Boats and Streams MCQ Current Affairs June 2017 MCQ Blood Relation MCQ Banking MCQ Electric Current MCQ Machine Input MCQ Surds and Indices MCQ Articles MCQ

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

Submit
Load More..
You can do it
  1. A compressor at high altitude will draw
  2. In jet engines, for the efficient production of large power, fuel is burnt in an atmosphere of
  3. The type of rotary compressor used in gas turbines, is of
  4. Which of the following statement is wrong?
  5. Phenomenon of choking in compressor means
  6. Compression efficiency is compared against
  7. The criterion of the thermodynamic efficiency for rotary compressor is
  8. The gas in cooling chamber of a closed cycle gas turbine is cooled at
  9. Which one of the following is the effect of blade shape on performance of a centrifugal compressor?
  10. A jet engine has
  11. In a jet propulsion unit, the products of combustion after passing through the gas turbine are discharged…
  12. A closed cycle gas turbine works on
  13. If infinite number of heaters be used in a gas turbine, then expansion process in turbine approaches
  14. Free air is the air at
  15. In a single acting reciprocating air compressor, without clearance, the compression of air may be
  16. The closed cycle in gas turbines
  17. Pick up the wrong statement
  18. Gas turbines use following type of air compressor
  19. Volumetric efficiency of a compressor decreases with ________ in compression ratio.
  20. The pressure ratio of an ideal vaned compressor with increase in mass flow rate
  21. In the aircraft propellers
  22. When the outlet angle from the rotor of a centrifugal compressor is more than 90°, then the blades…
  23. A closed gas turbine in which fuel is burnt directly in the air is not possible because of
  24. Fighter bombers use following type of engine
  25. Inter cooling in compressors
  26. Pick up the correct statement
  27. If the flow of air through the compressor is parallel to its axis, then the compressor is
  28. Volumetric efficiency of a compressor without clearance volume
  29. The absolute pressure of air at the outlet of a compressor is called
  30. A closed cycle gas turbine consists of a