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A finite element analysis of the exact nonlinear formulation of a lifting surface in steady incompressible flow, with the evaluation of the correct wake geometryThe problem of steady incompressible flow for lifting surfaces is considered. An integral equation is solved relating the values of the potential discontinuity on the lifting surface and its wake to the values of the normal derivative of the potential which are known from the boundary conditions. The lifting surface and the wake are divided into small quadrilateral surface elements. The values of the potential discontinuity and the normal derivative of the potential are assumed to be constant within each lifting surface element and equal to their values at the centroids of the lifting surface elements. This yields a set of linear algebraic equations. An iteration procedure is used to obtain the wake geometry: the velocities at the corner points of the wake elements are calculated and the wake streamlines are aligned to be parallel to the velocity vector. The procedure is repeated until convergence is attained.
Document ID
19760007991
Acquisition Source
Legacy CDMS
Document Type
Thesis/Dissertation
Authors
Suciu, E. O.
(Boston Univ. Boston, MA, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1975
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-146074
Report Number: NASA-CR-146074
Accession Number
76N15079
Funding Number(s)
CONTRACT_GRANT: NGR-22-004-030
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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