Flight test results on the stability and control of the F-15 Quiet Spike aircraft /

Bibliographic Details

Main Author:	Moua, Cheng M. (Author)
Corporate Author:	United States. National Aeronautics and Space Administration (sponsoring body.)
Format:	Government Document eBook
Language:	English
Published:	Edwards, CA : National Aeronautics and, Space Administration, Dryden Flight Research Center, [2012]
Series:	NASA technical memorandum ; 215978.
Subjects:	F-15 aircraft. Flight tests. Aircraft control. Aircraft stability. Supersonic flight. Sonic booms. Fuselages. Noses (forebodies) Computational fluid dynamics. Flight control.
Online Access:	https://purl.fdlp.gov/GPO/gpo32721