Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets
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Author
Contributions
- Wasserbauer, Joseph W. - Contributor
- United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch. - Contributor
Publication
1986 - For sale by the National Technical Information Service, Washington, D.C., District of Columbia
Language
English
Word Count
0 words, Guess
Page Count
0 pages
Physical Format
Microform
Identifiers
- Open LibraryOL18218668M
Subjects
Topics
Low speedJet enginesAir intakesAerodynamicsSupersonic inletsSupersonic aircraftJet engines -- Air intakesInternal compression inlets
Series Statement
- NASA technical paper -- 2557.
Other Editions
- Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets
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