Boundary-layer transition results from the F-16XL-2 supersonic laminar flow control experiment
An edition of Boundary-layer transition results from the F-16XL-2 supersonic laminar flow control experiment (1999)
By Laurie A. Marshall
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