Effects of external stores on the aerodynamic characteristics of a 60 ̊Delta-wing fighter model at Mach 1.60 to 2.87 /

Effects of external stores on the aerodynamic characteristics of a 60 ̊Delta-wing fighter model at Mach 1.60 to 2.87 /

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Bibliographic Details
Main Author:	Spearman, M. Leroy
Corporate Author:	United States National Aeronautics and Space Administration. Scientific and Technical Information Office
Other Authors:	Monta, William J, Monta, William J. (joint author)
Format:	Government Document Book
Language:	English
Published:	[Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1977 [Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; for sale by the National Technical Information Service, 1977
Series:	NASA technical memorandum 74090
Subjects:	Aerodynamics, Hypersonic Fighter planes > Testing Fighter planes Stability of airplanes, Lateral Stability of airplanes, Longitudinal
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Call Number:	ISIL:US-CST MARCIVE NAS 1.15:74090 NASA TM 74090