3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
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Author
Contributions
- Saunders, J. D. - Contributor
- United States. National Aeronautics and Space Administration. - Contributor
Publication
1995 - National Technical Information Service, distributor, Washington, DC, District of Columbia
Language
English
Word Count
0 words, Guess
Page Count
0 pages
Physical Format
Microform
Identifiers
- OCLC Control Number35282961
- Open LibraryOL17106503M
Alternate Titles
- 3D Navier Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet.
Subjects
Series Statement
- NASA technical memorandum -- 107123.
Other Editions
- 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
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