Flow separation in shock wave boundary layer interactions at hypersonic speeds
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Author
Contributions
- Joint Institute for Advancement of Flight Sciences. - Contributor
- Langley Research Center. - Contributor
Publication
1990 - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, Washington, D.C, District of Columbia
Language
English
Word Count
0 words, Guess
Page Count
0 pages
Physical Format
Microform
Identifiers
- Open LibraryOL16126865M
Subjects
Series Statement
- NASA contractor report -- 4274.
- NASA contractor report -- NASA CR-4274.
Links
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