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Subsonic investigation of leading-edge flaps designed for vortex- and attached-flow on a high-speed civil transport configuration / Bryan A. Campbell [and three others].

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Format:
Book
Government document
Author/Creator:
Campbell, Bryan A., author.
Contributor:
Langley Research Center, issuing body.
Series:
NASA technical memorandum ; 1999-209701.
NASA/TM ; 1999-209701
Language:
English
Genre:
Online resources.
Physical Description:
1 online resource (103 pages) : illustrations.
Place of Publication:
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, December 1999.
Notes:
"December 1999."
"Performing organization: NASA Langley Research Center"--Report documentation page.
Includes bibliographical references (pages 102-103).
Online resource; title from PDF title page (NASA, viewed Sep. 14, 2017).
Other Format:
Microfiche version: Subsonic investigation of leading-edge flaps designed for vortex- and attached-flow on a high-speed civil transport configuration
OCLC:
1003643373

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