Experiments in aircraft roll-yaw control using forebody tangential blowing
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Author
Contributions
- Joint Institute for Aeronautics and Acoustics. - Contributor
Publication
1997 - Joint Institute for Aeronautics and Acoustics, Stanford University, Stanford, Calif., California
Language
English
Word Count
0 words, Guess
Page Count
0 pages
Physical Format
Microform
Identifiers
- Open LibraryOL15545010M
Alternate Titles
- Experiments in aircraft roll yaw control using forebody tangential blowing.
Subjects
Series Statement
- JIAA TR -- 120.
- [NASA contractor report] -- NASA/CR-208349.
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