Static investigation of a two-dimensional convergent-divergent exhaust nozzle with multiaxis thrust-vectoring capability
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Author
Contributions
- United States. National Aeronautics and Space Administration. Scientific and Technical Information Division. - Contributor
Publication
1990 - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, Washington, DC, District of Columbia
Language
English
Word Count
0 words, Guess
Page Count
0 pages
Physical Format
Microform
Identifiers
- Open LibraryOL15368336M
Subjects
Series Statement
- NASA technical paper -- 2973.
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