Subsonic investigation of leading-edge flaps designed for vortex- and attached-flow on a high-speed civil transport configuration
By: Bryan A. Campbell ... [et al.].
Contributors: Campbell, Bryan A.; Langley Research Center.
Series: NASA/TM -- 1999-209701.; NASA technical memorandum -- 209701.
Publisher: National Aeronautics and Space Administration, Langley Research Center; Available from NASA Center for Aerospace Information; National Technical Information Service [distributor
Published: 1999
Place of publication: Hampton, Va; Hanover, MD; Springfield, VA
Language: eng
Format: Microform
Subjects: Subsonic wind tunnels.; Leading edge flaps.; Vortices.; Supersonic transports.; Aerodynamic configurations.; Separated flow.
Other titles: Subsonic investigation of leading edge flaps designed for vortex- and attached-flow on a high-speed civil transport configuration.
Notes: Shipping list no.: 2000-0596-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 2000] 2 microfiches.