Ira J. Walker

Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0

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Author

Ira J. Walker

Contributions

Covell, Peter F. - Contributor
Forrest, Dana K. - Contributor
United States. National Aeronautics and Space Administration. Scientific and Technical Information Program. - Contributor

Publication

1993 - National Technical Information Service, distributor], Washington, DC, District of Columbia

Language

English

Word Count

0 words, Guess

Page Count

0 pages

Physical Format

Microform

Identifiers

Open LibraryOL15403234M

Subjects

Topics

Mach number Delta wings Hypersonics Tail assemblies Wind tunnel tests Research vehicles Hypersonic vehicles

Series Statement

NASA technical memorandum -- 4413.

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