F-18 High Alpha Research Vehicle surface pressures
Subtitle: initial in-flight results and correlation with flow visualization and wind-tunnel data
By: David F. Fisher, Daniel W. Banks, David M. Richwine.
Contributors: Banks, Daniel W.; Richwine, David M.; Dryden Flight Research Facility.; AIAA Applied Aeronautics Conference ( 8th : 1990 : Portland, Oregon.)
Series: NASA technical memorandum -- 101724.
Publisher: NASA Ames Resarch Center, Dryden Flight Research Facility; National Technical Information Service, distributor]
Published: 1990
Place of publication: Edwards, Calif; [Springfield, Va
Language: eng
Format: Microform
Number of pages: 36
Subjects: Aerodynamic load.; Flow visualization.; Angle of attack.; F-18 aircraft.; Flight tests.; Forebodies.; Leading edges.; Mach number.; Pressure distribution.; Wind tunnel tests.
Notes: Shipping list no.: 1991-0796-M.

Distributed to depository libraries in microfiche.

"August 1990."

Prepared as AIAA 90-3018 for presentation at the AIAA 8th Aerodynamics Confernce, Portland, Oregon, August 20-22, 1990.

Includes bibliographical references (p. 9).

Also available via Internet from the NTRS web site. Address as of 1/17/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19910009738%5F1991009738.pdf; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration,] 1991. 1 microfiche.