Flight demonstration of a shock location sensor using constant voltage hot-film anemometry

An edition of Flight demonstration of a shock location sensor using constant voltage hot-film anemometry (1997)

Flight demonstration of a shock location sensor using constant voltage hot-film anemometry

By Timothy R. Moes

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Publish Date

1997

Publisher

National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program,National Technical Information Service, distributor]

Language

eng

Pages

Description:

subjects: F-15 aircraft, Hot-film anemometers, Airfoils, Laminar boundary layer, Leading edges, Pressure sensors, Transonic speed