Aerodynamic characteristics of a hypersonic research airplane concept having a 70̊ swept double-delta wing at Mach numbers from 1.50 to 2.86 / Jim A. Penland, Roger H. Fournier, and Don C. Marcum, Jr.

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Bibliographic Details
Main Author:	Penland, Jim A.
Corporate Authors:	Langley Research Center, United States. National Aeronautics and Space Administration
Other Authors:	Fournier, Roger H., Marcum, Don C.
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1975.
Series:	NASA technical note ; D-8065.
Subjects:	Aerodynamics, Supersonic. Hypersonic planes. Delta wing airplanes. Research aircraft.

Norlin Library - Government Information - US

Holdings details from Norlin Library - Government Information - US
Call Number:	NAS 1.14:D-8065
NAS 1.14:D-8065	Available Place a Hold