The application to airfoils of a technique for reducing orifice-induced pressure error at high Reynolds numbers
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Author
Contributions
- United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch. - Contributor
Publication
1986 - 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 LibraryOL17684311M
Series Statement
- NASA technical paper -- 2537.
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