Diamond shaped airfoil oriented to the oncoming stream

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Reference no: EM13713248

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?

Reference no: EM13713248

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