Effect of leading-edge load constraints on the design and performance of supersonic wings
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Author
Contributions
- United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch. - Contributor
Publication
1985 - For sale by the National Technical Information Service], Washington, DC, District of Columbia
Language
English
Word Count
0 words, Guess
Page Count
0 pages
Physical Format
Microform
Identifiers
- Open LibraryOL18029589M
Alternate Titles
- Effect of leading edge load constraints on the design and performance of supersonic wings.
Series Statement
- NASA technical paper -- 2446.
Other Editions
- Effect of leading-edge load constraints on the design and performance of supersonic wings
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