Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft /

Bibliographic Details

Main Author:	Steenken, William G. (Author)
Format:	Government Document eBook
Language:	English
Published:	Edwards, California : National Aeronautics and Space Administration, Dryden Flight Research Center, February 1999.
Series:	NASA technical memorandum ; 1999-206572.
Subjects:	F-18 aircraft. Aerodynamic stability. Angle of attack. Compressors. Control surfaces. Flight control. Research vehicles. Rotors. Subsonic speed.
Online Access:	https://purl.fdlp.gov/GPO/gpo83895