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Research in Natural Laminar Flow and Laminar-Flow Control, part 1Since the mid 1970's, NASA, industry, and universities have worked together to conduct important research focused at developing laminar flow technology that could reduce fuel consumption for general aviation, commuter, and transport aircraft by as much as 40 to 50 percent. The symposium was planned in view of the recent accomplishments within the areas of laminar flow control and natural laminar flow, and the potential benefits of laminar flow technology to the civil and military aircraft communities in the United States. Included were technical sessions on advanced theory and design tool development; wind tunnel and flight research; transition measurement and detection techniques; low and high Reynolds number research; and subsonic and supersonic research.
Document ID
19900003187
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Hefner, Jerry N.
(NASA Langley Research Center Hampton, VA, United States)
Sabo, Frances E.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1987
Subject Category
Aerodynamics
Report/Patent Number
L-16350-PT-1
NAS 1.55:2487-PT-1
NASA-CP-2487-PT-1
Report Number: L-16350-PT-1
Report Number: NAS 1.55:2487-PT-1
Report Number: NASA-CP-2487-PT-1
Accession Number
90N12503
Funding Number(s)
PROJECT: RTOP 505-60-31-06
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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