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New convergence criteria for the vortex-lattice models of the leading-edge separationThe convergence criterion for the vortex-lattice technique which deals with delta wings exhibiting significant leading-edge separation was studied. It was shown that one can predict pressure distributions without irregularities which agree fairly well with experimental data (which show some irregularities of their own) by replacing the system of discrete vortex lines with a single concentrated core. This core has a circulation equal to the algebraic sum of the circulations around the discrete lines and is located at the centroid of these lines. Moreover, there is a requirement that the position and strength of the core must converge as the number of elements increases. Because the calculation of the position and strength of the core is much less involved than the calculation of the loads, this approach has the additional desirable feature of requiring less computational time.
Document ID
19760021091
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kandil, O. A.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Mook, D. T.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Nayfeh, A. H.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1976
Publication Information
Publication: NASA. Langley Res. Center Vortex-Lattice Utilization
Subject Category
Aerodynamics
Accession Number
76N28179
Funding Number(s)
CONTRACT_GRANT: NSG-1262
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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