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Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0 [microform] / Ira J. Walker, Peter F. Covell And Dana K. Forrest.

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Bibliographic Details
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Main Author:	Walker, Ira J.
Corporate Author:	United States. National Aeronautics and Space Administration. Scientific and Technical Information Program
Other Authors:	Covell, Peter F., Forrest, Dana K.
Format:	Government Document Book
Language:	English
Published:	[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [National Technical Information Service, distributor], 1993.
Series:	NASA technical memorandum ; 4413.
Subjects:	Aerodynamic characteristics. Canard configurations. Delta wings. Hypersonic vehicles. Hypersonics. Mach number. Research vehicles. Stabilizers (Fluid dynamics) Tail assemblies. Wind tunnel tests.

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Norlin Library - Government Information - Microform

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Call Number:	NAS 1.15:4413
NAS 1.15:4413	Restricted Place a Hold

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Call Number:	NAS 1.15:4413
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