Pressure distributions from subsonic tests of a NACA 0012 semispan wing model

An edition of Pressure distributions from subsonic tests of a NACA 0012 semispan wing model (1995)

Pressure distributions from subsonic tests of a NACA 0012 semispan wing model

By Zachary T. Applin

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Publish Date

1995

Publisher

National Aeronautics and Space Administration, Langley Research Center,National Technical Information Service, distributor

Language

eng

Pages

Description:

subjects: Aerodynamic configurations, Airfoil profiles, Dynamic pressure, Free flow, Pressure distribution, Semispan models, Subsonic speed, Unswept wings, Wind tunnel tests