Subsonic investigation of a leading-edge boundary layer cont[r]ol suction system on a high-speed civil transport configuration /

Subsonic investigation of a leading-edge boundary layer cont[r]ol suction system on a high-speed civil transport configuration /

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Bibliographic Details
Corporate Author: Langley Research Center
Other Authors: Campbell, Bryan A
Format: Government Document Book
Language:English
Published: Hampton, Va. : Hanover, MD : Springfield, VA : National Aeronautics and Space Administration, Langley Research Center ; Available from NASA Center for Aerospace Information ; National Technical Information Service [distributor], [1999]
Series:NASA technical memorandum 209700
Subjects:
Boundary layer control
Aerodynamic configurations
Flaps (Control surfaces)
Leading edges
Pressure effects
Subsonic speed
Supersonic transports
Wind tunnel tests

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Stanford University

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Call Number: NAS 1.15:209700

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