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A potential-flow/boundary layer method for calculating subsonic and transonic airfoil flow with trailing-edge separation

A potential-flow/boundary layer method for calculating subsonic and transonic airfoil flow with trailing-edge separation

By Richard W Barnwell

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Publish Date

1981

Publisher

National Aeronautics and Space Administration, Scientific and Technical Information Branch,For sale by the National Technical Information Service]

Language

eng

Pages

37