Subsonic investigation of a leading-edge boundary layer cont[r]ol suction system on a high-speed civil transport configuration
By: Bryan A. Campbell ... [et al.].
Contributors: Campbell, Bryan A.; Langley Research Center.
Series: NASA/TM -- 1999-209700.; NASA technical memorandum -- 209700.
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: Boundary layer control.; Leading edges.; Wind tunnel tests.; Flaps (Control surfaces); Pressure effects.; Subsonic speed.; Supersonic transports.; Aerodynamic configurations.
Other titles: Subsonic investigation of a leading edge boundary layer control suction system 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.