Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method

An edition of Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method (1996)

Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method

EUROMECH-Colloquium 349, simulation of fluid-structure interaction in aeronautics, Göttingen, Germany, September 16-18, 1996

By Euromech Colloquium (349th 1996 Göttingen, Germany)

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Publish Date

1996

Publisher

National Aeronautics and Space Administration,National Technical Information Service, distributor

Language

eng

Pages

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