Theoretical/numerical study of feasibility of use of winglets on low aspect ratio wings at subsonic and transonic Mach numbers to reduce drag
By: John M. Kuhlman, Paul Liaw, and Michael J. Cereney.
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
Series: NASA contractor report -- 4174.; NASA contractor report -- NASA CR-4174.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Division; For sale by the National Technical Information Service]
Published: 1988
Place of publication: [Washington, DC]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Aerodynamics, Transonic.; Drag (Aerodynamics)
Other titles: Theoretical numerical study of feasibility of use of winglets on low aspect ratio wings at subsonic and transonic Mach numbers to reduce drag.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1988. 1 microfiche.