Inlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60 ° angle of attack /

Bibliographic Details

Main Author:	Walsh, Kevin R. (Author)
Corporate Authors:	Analytical Services & Materials, Inc, GE Aircraft Engines (Firm), United States. National Aeronautics and Space Administration (sponsoring body.)
Format:	Government Document eBook
Language:	English
Published:	Edwards, California : National Aeronautics and Space Administration, Dryden Flight Research Center, April 1997.
Series:	NASA technical memorandum ; 104329.
Subjects:	F-18 aircraft. Angle of attack. Aerodynamic characteristics. Pressure recovery. Engine inlets.
Online Access:	https://purl.fdlp.gov/GPO/gpo66657