Consider the isentropic flow on the airfoil. The free-flow condition is At a certain point on the

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Consider the isentropic flow on the airfoil. The free-flow condition isimage text in transcribedimage text in transcribed

At a certain point on the airfoil, the pressure is 3.6 × 104 N/m2. Calculate the density at this point.

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Aerodynamics

ISBN: 9789811945861

1st Edition

Authors: Peiqing Liu

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