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Total No. of Questions : 09
B.Tech.(Aerospace Engg.) (2012 Onwards)
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AEROELASTICITYSubject Code : ASPE-402
M.Code : 72565
Total No. of Pages : 02
(Sem.-7,8)
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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 :
- Aeroelasticity
- Weighting matrices
- Flutter
- Model scale factors
- Control reversal
- Influence coefficients
- Aileron effectiveness
- Degree of freedom
- Divergence
- Dynamic loads
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SECTION-B
- Explain vibration model similarity laws.
- Explain the phenomenon of wing torsional divergence for finite wing case.
- What are aeroelastic instabilities and how can these instabilities be prevented?
- Define Critical Flutter Speed. How is critical flutter speed determined?
- Explain steady state aeroelastic model testing.
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SECTION-C
- Write notes on the following :
- Flight flutter testing
- Structural simulations
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- Write and explain the significance of differential form of equation of motion of vibrations. Discuss the natural modes and frequencies of complex airplane structures.
- Write notes on the following :
- Identification and measurement of normal modes
- Coupling of bending and torsional oscillations
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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)