Cover Image

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
Description
Item Description:Title from title screen (viewed April 5, 2016).
"June 1997."
"Performing organization: NASA Dryden Flight Research Center, Edwards, California"--Report documentation page.
Physical Description:1 online resource (v, 850 pages) : illustrations.
Bibliography:Includes bibliographical references (pages 849-850).