Surface pressure data for a supersonic-cruise airplane configuration at mach numbers of 2.30, 2.96, and 3.30
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Author
Contributions
- Corlett, William A - Contributor
- Collins, Ida K - Contributor
- United States. National Aeronautics and Space Administration. Scientific and Technical Information Office - Contributor
- Langley Research Center - Contributor
Publication
1979 - For sale by the National Technical Information Service], Greeenbelt, Md, District of Columbia
Language
English
Subjects
Series Statement
- NASA technical memorandum -- 80061
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