Previous Year Very Short Questions of AT (B-TECH automobile engineering 3rd)

Applied thermodynamics

Previous year question paper with solutions for Applied thermodynamics

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  1. On what factors, volumetric efficiency of a compressor depends?
  2. Why aerofoil blading is needed in axial flow compressor?
  3. What is propulsion efficiency?
  4. Define the term thrust and thrust power of jet propulsion system
  5. State the assumptions made in practical cycle analysis in gas turbine.
  6. Enumerate the applications of compressed air.
  7. What do you understand by blade efficiency?
  8. What is a turboprop engine?
  9. What is a heat exchanger?
  10. Why intercooling is done?
  11. List four applications of compressed air.
  12. What is polytropic efficiency?
  13. What is the difference in the working principle of positive displacement compressors and dynamic compressors?
  14. Draw the p-V diagram for a double stage reciprocating compressor with and without inter cooling
  15. What is the function of a diffuser in a centrifugal compressor?
  16. Why the blades of an axial flow compressor are of airfoil section?
  17. Explain the terms slip factor and power input factor as applied to centrifugal compressor.
  18. List four advantages of gas turbines over I.C engines.
  19. Write briefly the applications of a gas turbine.
  20. What is the working principle of jet propulsion?
  21. Represent isothermal, isentropic and polytropic compression process on P-V diagram.
  22. Write formula for indicated power for single acting and double acting reciprocating compressor
  23. What is effect of clearance on volumetric efficiency in reciprocating compressor?
  24. What is function of diffuser in centrifugal compressor?
  25. For which requirements, centrifugal compressors are used?
  26. Define degree of reaction in axial flow compressors.
  27. Draw ideal and actual cycle for gas turbine on T-S diagram
  28. Define cycle air rate in gas turbine.
  29. Write two advantages of jet propulsion system
  30. Write basic difference between turbojet and turboprop.