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Hypersonic Aerodynamics MCQ
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The term "stagnation temperature" refers to:
The term "stagnation temperature" refers to:
A. Temperature at zero velocity point in flow
B. Ambient temperature
C. Combustion chamber temperature
D. Engine exit temperature
Explanation:
Stagnation temperature is the temperature the flow would reach if brought to rest isentropically.
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Hypersonic Aerodynamics MCQ
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Aerospace Engineering
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