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

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

-

1-2 of 2 Editions

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

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

Language: eng

Published In: 1995

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

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

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

Language: eng

Published In: 1995

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