Effects of wing sweep on boundary-layer transition for a smooth F-14A wing at Mach numbers from 0.700 to 0.825

An edition of Effects of wing sweep on boundary-layer transition for a smooth F-14A wing at Mach numbers from 0.700 to 0.825 (1990)

Effects of wing sweep on boundary-layer transition for a smooth F-14A wing at Mach numbers from 0.700 to 0.825

By Bianca T. Anderson

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Publish Date

1990

Publisher

National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility,For sale by the National Technical Information Service

Language

eng

Pages

Description:

subjects: Laminar flow, Boundary layer transition, Variable sweep wings, Mach number, Flow distribution