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Overview of the Langley viscous drag reduction programAs a result of reductions in form drag and roughness drag, skin friction, drag, or viscous drag now represents a major contributor to the cruise drag of subsonic business and transport aircraft, and hence, is considered a barrier problem to further significant improvements in the aerodynamic efficiency of these aircraft. To meet the challenge, research in the areas of laminar-flow control and turbulence control/drag reduction was initiated at NASA Langley Research Center. The significance of this research is discussed.
Document ID
19880005564
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Hefner, Jerry N.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
December 1, 1986
Publication Information
Publication: Langley Symposium on Aerodynamics, Volume 1
Subject Category
Aerodynamics
Accession Number
88N14946
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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