When Ma of an airfoil increases to 0.8, the velocity of the maximum velocity point on the
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When Ma∞ of an airfoil increases to 0.8, the velocity of the maximum velocity point on the airfoil reaches the sound velocity. What is the pressure coefficient of the airfoil at the maximum speed point at low speed? It is assumed that the Prandtl–Glauert rule is available.
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