1.

On which of this parameter is the coefficient of lift over a two – dimensional body at hypersonic flow dependent?

A. γ.\(\frac {α}{τ}\)
B. γ, K, M∞
C. M∞T, \(\frac {α}{τ}\), γ
D. M∞T, K, γ
Answer» D. M∞T, K, γ


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