Computational test cases for a clipped delta wing with pitching and trailing-edge control surface oscillations

An edition of Computational test cases for a clipped delta wing with pitching and trailing-edge control surface oscillations (1999)

Computational test cases for a clipped delta wing with pitching and trailing-edge control surface oscillations

By Robert M. Bennett

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Publish Date

1999

Publisher

National Aeronautics and Space Administration, Langley Research Center,National Technical Information Service, distributor

Language

eng

Pages

Description:

subjects: Computational fluid dynamics, Pitch (Inclination), Airfoil profiles, Delta wings, Control surfaces, Wind tunnel tests