Roll No.
Total No. of Questions : 09
Total No. of Pages : 02
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B.Tech.(Aerospace Engg.) (2012 Onwards) (Sem.-4)
AEROSPACE PROPULSION-I
Subject Code : ASPE-207
M.Code: 71531
Time: 3 Hrs.
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Max. Marks : 60
INSTRUCTIONS 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
- Answer briefly :
- Name two types of gas turbine engines which primarily provides shaft power output.
- Write thrust equation for a jet engine which is operating at fully expanded nozzle condition.
- How is an isentropic flow different from an adiabatic flow?
- Define total pressure.
- Which thermodynamic cycle does a gas turbine works on?
- Write the relation for isentropic efficiency of a compressor.
- Which thrust augmentation is utilized during take-off in hot weather?
- Name any 4 categories of rocket engine types based on propellants.
- What is uninstalled thrust?
- What is the maximum achievable exit Mach number in convergent nozzle?
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SECTION-B
- Obtain thrust equation for a rocket engine.
- Mention the property variation across an oblique shock on a neat diagram.
- For isentropic flow, obtain the relation for pressure ratio vs temperature ratio.
- Show that the least pressure ratio required across a nozzle to reach sonic speed is 1.89.
- Briefly explain about any two parameters affecting the takeoff thrust of an engine.
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SECTION-C
- Classify aircraft engines based on their operational flight Mach no. and explain their limitations.
- With neat diagram, explain the various configurations of solid propellant structures and state their advantages.
- Explain the over expanded and under expanded rocket nozzle operating conditions with help of a neat diagram.
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 4th Semester Last 10 Years 2009-2019 Previous Question Papers|| Punjab Technical University
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