Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel

An edition of Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel (1985)

Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel

By William G. Johnson

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Publish Date

1985

Publisher

National Aeronautics and Space Administration, Scientific and Technical Information Branch,For sale by the National Technical Information Service]

Language

eng

Pages

Description:

subjects: Aerodynamics, Transonic, Aerofoils, Airfoil profiles, Boeing aircraft, Cryogenic wind tunnels, High Reynolds number, Pressure distribution, Reynolds number, Statistics, Supercritical airfoils, Testing, Transonic Aerodynamics, Two dimensional bodies, Wind tunnel models, Wind tunnel tests