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Roll No. Total No. of Pages : 02
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Total No. of Questions : 09B.Tech.(Aerospace Engg.) (2012 Onwards) (Sem.-4)
AEROSPACE PROPULSION -1
Subject Code : ASPE-207
M.Code : 71531
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Time : 3 Hrs. Max. Marks : 60INSTRUCTIONS TO CANDIDATES :
- SECTION-A is COMPULSORY consisting of TEN questions carrying TWO marks each.
- SECTION-B contains FIVE questions carrying FIVE marks each and students have to attempt any FOUR questions.
- SECTION-C contains THREE questions carrying TEN marks each and students have to attempt any TWO questions.
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SECTION-A
- Write briefly :
- What is S.T.O.L?
- Define isentropic efficiency.
- What is Scramjet?
- Write the thrust equation of a rocket.
- Define total impulse for a rocket.
- What is Rocket propulsion?
- Write the expression for propulsive efficiency of a jet engine.
- Define grain with reference to a solid propellant.
- What is a Trivial flow?
- What is a over expanded nozzle?
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SECTION-B
- Discuss simple compressible system and equation of state.
- Discuss simple frictional flow and plot a fanno line.
- Draw a Brayton cycle on T — S diagram and write the expression for specific work output.
- Discuss and explain the working of a Turboprop engine.
- Draw a figure of solid propellant motor and explain its working.
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SECTION-C
- Name various types of missiles and discuss about their structures. What is the significance of heat transfer and cooling system in a Rocket?
- Discuss static performance of a Rocket in details.
- Discuss the performance of both single and multistage rockets. Write the various applications of Rockets.
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NOTE : Disclosure of Identity by writing Mobile No. or Making of passing request on any page of Answer Sheet will lead to UMC against the Student.
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This download link is referred from the post: PTU B.Tech Question Papers 2020 March (All Branches)
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