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Aerospace Engineering
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Hypersonic Aerodynamics MCQ
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The shock layer thickness decreases with:
The shock layer thickness decreases with:
A. Increase in Mach number
B. Decrease in altitude
C. Increase in vehicle size
D. Increase in air temperature
Explanation:
Higher Mach numbers lead to thinner shock layers.
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Hypersonic Aerodynamics MCQ
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Aerospace Engineering
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