Transient flow thrust prediction for an ejector propulsion concept
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Author
Contributions
- United States. National Aeronautics and Space Administration. - Contributor
Publication
1989 - 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
- Open LibraryOL15294123M
Subjects
Topics
EjectorsJet propulsionVertically rising aircraftUnsteady flow (Fluid dynamics)Vertically rising aircraft -- Jet propulsion -- Ejectors
Series Statement
- NASA technical memorandum -- 102078.
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