Consider a diamond shaped airfoil oriented to the oncoming


Consider a diamond shaped airfoil oriented to the oncoming stream. Approximate results since the inclination angles are small. All four faces are same length. Angle of attack is 10 deg

a) According to Newtonian hypersonic theory, Find the numerical value of lift coefficient. Assume pressure is zero on the downstream face

b) According to ideal fluid theory, what is the drag coefficient?

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Mechanical Engineering: Consider a diamond shaped airfoil oriented to the oncoming
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