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.; United States. National Aeronautics and Space Administration.
Series: NASA/TM -- 1999-209013; NASA technical memorandum -- 1999-209013.
Publisher: National Aeronautics and Space Administration, Dryden Flight Research Center; Available from NASA Center for AeroSpace Information
Published: 1999
Place of publication: Edwards, Calif; Hanover, Md
Language: eng
Number of pages: 48
Subjects: Aerodynamics, Supersonic.; Boundary layer.; F-16 (Jet fighter plane); Laminar flow.
Notes: "December 1999."

"Performing organization report number H-2382"--Report documentation page.

Includes bibliographical references.

Prepared by NASA Dryden Flight Research Center for the National Aeronautics and Space Administration WU 522 31 24 00 24 00 SLF