Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing
By: Sheryll Goecke Powers and Lannie D. Webb.
Contributors: Webb, Lannie D.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Program.; United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 4789.
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program; National Technical Information Service, distributor]
Published: 1997
Place of publication: [Washington, D.C.]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Flight tests.; Boundary layers.; Swept wings.; Pressure distribution.; Mach number.; Angle of attack.; Reynolds number.; Supercritical wings.; Pressure measurement.
Notes: Shipping list no.: 99-0685-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 9 microfiches.