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Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing

Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing

By Thomas A Byrdsong

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Publish Date

1983

Publisher

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

Language

eng

Pages

193

Description: