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An application of the suction analog for the analysis of asymmetric flow situationsA recent extension of the suction analogy for estimation of vortex loads on asymmetric configurations is reviewed. This extension includes asymmetric augmented vortex lift and the forward sweep effect on side edge suction. Application of this extension to a series of skewed wings has resulted in an improved estimating capability for a wide range of asymmetric flow situations. Hence, the suction analogy concept now has more general applicability for subsonic lifting surface analysis.
Document ID
19770003408
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Luckring, J. M.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1976
Publication Information
Publication: Advan. in Eng. Sci., Vol. 4
Subject Category
Aerodynamics
Accession Number
77N10350
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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