At low speeds, the minimum pressure coefficient on the top surface of the airfoil is –o.90. What is the critical Mach number of the airfoil?
1. Consider an airfoil at a given angle of attack, say a1• At low speeds, the minimum pressure coefficient on the top surface of the airfoil is –o.90. What is the critical Mach number of the airfoil? 2. Consider the airfoil in Prob. 5.15 at a smaller angle of attack, say ~.At low speeds, the minimum pressure coefficient is – 0.65 at this lower angle of attack. What is the critical Mach number of the airfoil? Prob. 5.15 Consider an airfoil at a given angle of attack, say a1• At low speeds, the minimum pressure coefficient on the top surface of the airfoil is –o.90. What is the critical Mach number of the airfoil?
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