Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft
By: W.G. Steenken ... [et al.].
Contributors: Steenken, W. G.; Hugh L. Dryden Flight Research Center.; United States. National Aeronautics and Space Administration.
Series: NASA/TM -- 1999-206572; NASA technical memorandum -- 206572..
Publisher: National Aeronautics and Space Administration, Dryden Flight Research Center; National Technical Information Service, distributor
Published: 1999
Place of publication: Edwards, Calif; Springfield, VA
Language: eng
Format: Microform
Subjects: F-18 aircraft.; Aerodynamic stability.; Angle of attack.; Compressors.; Control surfaces.; Flight control.; Research vehicles.; Rotors.; Subsonic speed.
Other titles: Factors affecting inlet engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft
Notes: Shipping list no.: 99-0685-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1999] 3 microfiches.