Dynamic response of a forward-swept-wing model at angles of attack up to 15 at a Mach number of 0.8
By: Robert V. Doggett, Jr., and Rodney H. Ricketts
Contributors: Ricketts, Rodney H; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch; Langley Research Center (U.S.)
Series: NASA technical memorandum -- 81863
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1980
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 28
Subjects: Airplanes -- Wings; Aeroelasticity; Buffeting (Aerodynamics)
Notes: "Langley Research Center."

Nov. 1980

Includes bibliographical references