A potential-flow/boundary layer method for calculating subsonic and transonic airfoil flow with trailing-edge separation
By: Richard W. Barnwell
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch; Langley Research Center
Series: NASA technical memorandum -- 81850
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1981
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 37
Subjects: Aerofoils -- Mathematical models; Turbulent boundary layer -- Mathematical models; Aerodynamics, Transonic
Notes: "Langley Research Center."

"June 1981"--Cover

Subject Category 02

Includes bibliographical references