Calculation of vortex lift effect for cambered wings by the suction analogy
By: C. Edward Lan and Jen-Fu Chang ; prepared for Langley Research Center under grant NSG-1629
Contributors: Chang, Jen-Fu; Langley Research Center; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch; University of Kansas. Center for Research
Series: NASA contractor report -- 3449
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: 83
Subjects: Lift (Aerodynamics); Camber (Aerofoils)
Notes: "The University of Kansas Center for Research, Inc."

"July 1981"--Cover

Includes bibliographical references