A potential-flow/boundary layer method for calculating subsonic and transonic airfoil flow with trailing-edge separation
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Author
Contributions
- United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch. - Contributor
- Langley Research Center. - Contributor
Publication
1981 - For sale by the National Technical Information Service], Washington, D.C, District of Columbia
Language
English
Subjects
Topics
AerofoilsTransonic AerodynamicsAerodynamics, TransonicTurbulent boundary layerAerofoils -- Mathematical modelsTurbulent boundary layer -- Mathematical models
Places
Series Statement
- NASA technical memorandum -- 81850.
Other Editions
- A potential-flow/boundary layer method for calculating subsonic and transonic airfoil flow with trailing-edge separation
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