[PDF.45kd] Aerodynamic Characteristics at Reynolds Numbers of 3.0 x 10(6) and 6.0 x10(6) of Three Airfoil Sections Formed by Cutting Off Various Amounts From the Rear Portion of the NACA 0012 Airfoil Section
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Aerodynamic Characteristics at Reynolds Numbers of 3.0 x 10(6) and 6.0 x10(6) of Three Airfoil Sections Formed by Cutting Off Various Amounts From the Rear Portion of the NACA 0012 Airfoil Section
Hamilton A. Smith
[PDF.wg71] Aerodynamic Characteristics at Reynolds Numbers of 3.0 x 10(6) and 6.0 x10(6) of Three Airfoil Sections Formed by Cutting Off Various Amounts From the Rear Portion of the NACA 0012 Airfoil Section
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