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A finite-element method for lifting surfaces in steady incompressible subsonic flowThe problem of potential steady subsonic flow for lifting surfaces is considered. This problem requires the solution of an integral equation relating the value 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 is divided into small (quadrilateral hyperboloidal) surface elements, which are described in terms of the Cartesian components of the four corner points. The values of the potential discontinuity and the normal derivative of the potential are assumed to be constant within each element and equal to their values at the centroids of the elements. This yields a set of linear algebraic equations. Numerical results are in good agreement with existing ones.
Document ID
19750015405
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Morino, L.
(Boston Univ. Boston, MA, United States)
Suciu, E. O.
(Boston Univ. Boston, MA, United States)
Date Acquired
September 3, 2013
Publication Date
December 1, 1974
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-142811
TR-74-05
Report Number: NASA-CR-142811
Report Number: TR-74-05
Accession Number
75N23477
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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