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A study of high-lift airfoils at high Reynolds numbers in the Langley Low-Turbulence Pressure Tunnel

study of high-lift airfoils at high Reynolds numbers in the Langley Low-Turbulence Pressure Tunnel

By Harry L. Morgan

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Publish Date

1989

Publisher

National Aeronautics and Space Administration, Scientific and Technical Information Office

Language

eng

Pages

-

Description:

subjectsReynolds number,  Aerofoils