Calculation of vortex lift effect for cambered wings by the suction analogy
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Author
Contributions
- Chang, Jen-Fu - Contributor
- Langley Research Center - Contributor
- United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch - Contributor
- University of Kansas. Center for Research - Contributor
Publication
1981 - For sale by the National Technical Information Service], Washington, D.C, District of Columbia
Language
English
Subjects
Topics
Camber (Aerofoils)Lift (Aerodynamics)
Series Statement
- NASA contractor report -- 3449
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