Body and canard effects on an attached-flow maneuver wing at Mach 1.62

An edition of Body and canard effects on an attached-flow maneuver wing at Mach 1.62 (1984)

Body and canard effects on an attached-flow maneuver wing at Mach 1.62

By Jimmy L Pittman

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Publish Date

1984

Publisher

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

Language

eng

Pages

145

Description:

subjects: Aerodynamics, Supersonic, Airplanes, Canard Wings, Supersonic Aerodynamics, Wings, Canard