The pressure coefficient distribution at on the airfoil measured in the low speed wind tunnel is shown

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The pressure coefficient distribution at on the airfoil measured in the low speed wind tunnel is shown below. Based on these infor-mation, estimat that the Critical Mach number of the NACA0012 airfoil at zero angle of attack.

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Aerodynamics

ISBN: 9789811945861

1st Edition

Authors: Peiqing Liu

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Question Posted: Sep 20, 2024 06:01 AM

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The pressure coefficient distribution at on the airfoil measured in the low speed wind tunnel is shown

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Re 3.65 x 106

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Aerodynamics

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