A low speed wind tunnel investigation of Reynolds number effects on a 60-deg. swept wing configuration with leading and trailing edge flaps
By: Dhanvada M. Rao and Keith D. Hoffler.
Contributors: Hoffler, Keith D.; Langley Research Center.
Series: NASA contractor report -- 181684.; NASA contractor report -- NASA CR-181684.
Publisher: National Aeronautics and Space Administration, Langley Research Center
Published: 1988
Place of publication: Hampton, Va
Language: eng
Format: Microform
Subjects: Airplanes -- Wings -- Testing.; Aerodynamics.
Notes: Distributed to depository libraries in microfiche.

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