Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing /

Bibliographic Details

Main Authors:	Powers, Sheryll Goecke (Author), Webb, Lannie D. (Author)
Corporate Authors:	NASA Dryden Flight Research Center, United States. National Aeronautics and Space Administration (sponsoring body.)
Format:	Government Document eBook
Language:	English
Published:	[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, June 1997.
Series:	NASA technical memorandum ; 4789.
Subjects:	Boundary layers. Pressure distribution. Supercritical wings. F-111 aircraft. Wing camber.
Online Access:	https://purl.fdlp.gov/GPO/gpo65701