Dynamic ground-effect measurements on the F-15 STOL and Maneuver Technology Demonstrator (S/MTD) configuration
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Author
Contributions
- United States. National Aeronautics and Space Administration. Scientific and Technical Information Division. - 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
7,000 words, Guess
Page Count
28 pages
Physical Format
Microform
Identifiers
- Open LibraryOL18257141M
Subjects
Series Statement
- NASA technical paper -- 3000.
Links
Other Editions
- Dynamic ground-effect measurements on the F-15 STOL and Maneuver Technology Demonstrator (S/MTD) configuration
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