Water tunnel flow visualization study of a 4.4% scale X-31 forebody

An edition of Water tunnel flow visualization study of a 4.4% scale X-31 forebody (1994)

Water tunnel flow visualization study of a 4.4% scale X-31 forebody

By Brent R. Cobleigh

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Publish Date

1994

Publisher

National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility,National Technical Information Service, distributor

Language

eng

Pages

Description:

subjects: X-31 aircraft, Strakes, Vortices, Forebodies, Angle of attack, Asymmetry, Flow visualization, Water tunnel tests