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Boundary-layer transition results from the F-16XL-2 supersonic laminar flow control experiment

Boundary-layer transition results from the F-16XL-2 supersonic laminar flow control experiment

By Laurie A. Marshall

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Publish Date

1999

Publisher

National Aeronautics and Space Administration, Dryden Flight Research Center,NASA Center for AeroSpace Information [distributor],National Technical Information Service [distributor

Language

eng

Pages

48