Static internal performance of a nonaxisymmetric vaned thrust reverser with flow splay capability
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Author
Contributions
- Leavitt, Laurence D. - Contributor
- United States. National Aeronautics and Space Administration. Scientific and Technical Information Division. - Contributor
Publication
1989 - 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 LibraryOL16124006M
Subjects
Topics
TestingDeflectorsJet planesStatic testsThrust reversalFlow deflectionThrust reversersWind tunnel testsThrust vector controlJet planes -- Thrust reversers -- Testing
Series Statement
- NASA technical paper -- 2933.
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