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Flight and wind-tunnel measurements showing base drag reduction provided by a trailing disk for high Reynolds number turbulent flow for subsonic and transonic Mach numbers

Flight and wind-tunnel measurements showing base drag reduction provided by a trailing disk for high Reynolds number turbulent flow for subsonic and transonic Mach numbers

By Sheryll Goecke Powers

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Publish Date

1988

Publisher

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

Language

eng

Pages

139