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

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Published 1999 by National Aeronautics and Space Administration, Langley Research Center, Available from NASA Center for Aerospace Information, National Technical Information Service [distributor in Hampton, Va, Hanover, MD, Springfield, VA .
Written in English

Subjects:

• Boundary layer control.,
• Leading edges.,
• Wind tunnel tests.,
• Flaps (Control surfaces),
• Pressure effects.,
• Subsonic speed.,
• Supersonic transports.,
• Aerodynamic configurations.

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Edition Notes

Other titles	Subsonic investigation of a leading edge boundary layer control suction system on a high-speed civil transport configuration.
Statement	Bryan A. Campbell ... [et al.].
Series	NASA/TM -- 1999-209700., NASA technical memorandum -- 209700.
Contributions	Campbell, Bryan A., Langley Research Center.
The Physical Object
Format	Microform
Pagination	1 v.
ID Numbers
Open Library	OL15568006M

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