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.
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.