Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code
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Author
Contributions
- Anderson, Bernhard H. - Contributor
- Shaw, Robert J. 1946- - Contributor
- United States. National Aeronautics and Space Administration. - Contributor
Publication
1994 - National Aeronautics and Space Administration, Washington, DC, District of Columbia
Language
English
Word Count
0 words, Guess
Page Count
0 pages
Physical Format
Microform
Identifiers
- OCLC Control Number32731299
- Open LibraryOL17788471M
Subjects
Series Statement
- NASA technical memorandum -- 106580.
Other Editions
- Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code
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