Forward-swept-wing configuration designed for high maneuverability by use of a transonic computational method
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Author
Contributions
- Mercer, Charles E. - Contributor
- United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch. - Contributor
Publication
1987 - National Aeronautics and Space Administration, Scientific and Technical Information Branch, Washington, D.C., District of Columbia
Language
English
Word Count
45,250 words, Guess
Page Count
181 pages
Physical Format
Microform
Identifiers
- Open LibraryOL18029111M
Alternate Titles
- Forward swept wing configuration designed for high maneuverability by use of a transonic computational method.
Subjects
Topics
Series Statement
- NASA technical paper -- 2628.
Other Editions
- Forward-swept-wing configuration designed for high maneuverability by use of a transonic computational method
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