Computational test cases for a rectangular supercritical wing undergoing pitching oscillations
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Author
Contributions
- Walker, Charlotte E. - Contributor
- Langley Research Center. - Contributor
Publication
1999 - National Technical Information Service, distributor, Hampton, Va, Virginia
Language
English
Word Count
0 words, Guess
Page Count
0 pages
Physical Format
Microform
Identifiers
- Open LibraryOL15548991M
Subjects
Topics
Aircraft partsWind tunnel testsWing oscillationsRectangular wingsSupercritical wingsUnsteady aerodynamicsComputational fluid dynamics
Series Statement
- [NASA technical memorandum] -- NASA/TM-1999-209130.
- NASA technical memorandum -- 209130.
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