Hypersonic Aerodynamics MCQ

Q1. Hypersonic flow is generally defined as flow with Mach number greater than:

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Q2. At hypersonic speeds, which phenomenon significantly affects aerodynamic heating?

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Q3. Which type of shock wave is commonly formed in front of a blunt body at hypersonic speeds?

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Q4. Hypersonic flow is dominated by:

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Q5. Which parameter is critical in designing thermal protection for hypersonic vehicles?

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Q6. The shock layer thickness decreases with:

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Q7. Which approximation is used for hypersonic small-disturbance theory?

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Q8. At hypersonic speeds, air behaves as:

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Q9. The aerodynamic center in hypersonic flow shifts:

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Q10. Which of the following increases wave drag in hypersonic vehicles?

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Q11. The shock-expansion theory is used for:

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Q12. Real gas effects in hypersonic aerodynamics become significant due to:

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Q13. The term "stagnation temperature" refers to:

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Q14. Hypersonic vehicles often use which nose shape to reduce heat loads?

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Q15. Which non-dimensional number is important for compressible hypersonic flows?

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Q16. Entropy layer in hypersonic flow develops due to:

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Q17. Aerodynamic heating is proportional to approximately:

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Q18. Hypersonic boundary layer may transition to turbulence due to:

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Q19. Shock-shock interactions can lead to:

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Q20. Hypersonic waverider vehicles are designed to:

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