Low-speed wind-tunnel study of the high-angle-of-attack stability and control characteristics of a cranked-arrow-wing fighter configuration
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Author
Contributions
- United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch. - Contributor
Publication
1984 - For sale by the National Technical Information Service], Washington, D.C, District of Columbia
Language
English
Word Count
9,000 words, Guess
Page Count
36 pages
Identifiers
- OCLC Control Number11125791
- Open LibraryOL17078357M
Subjects
Topics
WingsTestingFighter planesStability of airplanesFighter planes -- WingsStability of airplanes -- Testing
Series Statement
- NASA technical memorandum -- 85776
Other Editions
- Low-speed wind-tunnel study of the high-angle-of-attack stability and control characteristics of a cranked-arrow-wing fighter configuration
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