Boundary-layer transition results from the F-16XL-2 supersonic laminar flow control experiment
By: Laurie A. Marshall.
Contributors: Hugh L. Dryden Flight Research Center.
Series: [NASA technical memorandum] -- NASA/TM-1999-209013.; NASA technical memorandum -- 209013.
Publisher: National Aeronautics and Space Administration, Dryden Flight Research Center; NASA Center for AeroSpace Information [distributor]; National Technical Information Service [distributor
Published: 1999
Place of publication: Edwards, Calif; Hanover, MD; Springfield, VA
Language: eng
Format: Microform
Other titles: Boundary layer transition results from the F-16XL-2 supersonic laminar flow control experiment.
Notes: Shipping list no.: 2000-0415-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 2000] 1 microfiche.