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Vortex lift research: Early contributions and some current challengesThe trend towards slender wing aircraft for supersonic cruise and the early chronology of research directed towards their vortex-lift characteristics are briefly reviewed. An overview of the development of vortex-lift theoretical methods is presented, and some current computational and experimental challenges related to the viscous flow aspects of this vortex flow are discussed.
Document ID
19860017719
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Polhamus, E. C.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
July 1, 1986
Publication Information
Publication: Vortex Flow Aerodynamics, Vol. 1
Subject Category
Aerodynamics
Accession Number
86N27191
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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