Aerodynamic effect of strakes on two-dimensional tail boom models of OH-58A and OH-58D helicopters
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Author
Contributions
- United States. National Aeronautics and Space Administration. - Contributor
Publication
1990 - National Technical Information Service, distributor, Washington, DC, District of Columbia
Language
English
Word Count
0 words, Guess
Page Count
0 pages
Physical Format
Microform
Identifiers
- Open LibraryOL15405518M
Subjects
Topics
StrakesCross flowWind directionTail assembliesWind tunnel testshelicopter controlHelicopter controlHelicopter performance
Series Statement
- NASA technical memorandum -- 4248.
- AVSCOM technical report -- 90-B-010.
- AVSCOM technical report -- 90-B-10.
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