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Aerospace Engineering
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Hypersonic Aerodynamics MCQ
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The shock-expansion theory is used for:
The shock-expansion theory is used for:
A. Subsonic flow
B. Transonic flow
C. Supersonic and hypersonic flow over wedges
D. Incompressible flow
Explanation:
Shock-expansion theory analyzes supersonic/hypersonic flow over slender bodies.
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Hypersonic Aerodynamics MCQ
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Aerospace Engineering
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At hypersonic speeds, which phenomenon significantly affects aerodynamic heating?
Which type of shock wave is commonly formed in front of a blunt body at hypersonic speeds?
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