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A finite-element analysis for steady and oscillatory subsonic flow around complex configurationsThe problem of potential subsonic flow around complex configurations is considered. The solution is given of an integral equation relating the values of the potential on the surface of the body to the values of the normal derivative, which is known from the boundary conditions. The surface of the body is divided into small (hyperboloidal quadrilateral) surface elements, which are described in terms of the Cartesian components of the four corner points. The values of the potential (and its normal derivative) within each element is assumed to be constant and equal to its value at the centroid of the element. The coefficients of the equation are given by source and doublet integrals over the surface elements. Closed form evaluations of the integrals are presented. The results obtained with the above formulation are compared with existing analytical and experimental results.
Document ID
19750019225
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Chen, L. T.
(Boston Univ. Boston, MA, United States)
Suciu, E. O.
(Boston Univ. Boston, MA, United States)
Morino, L.
(Boston Univ. Boston, MA, United States)
Date Acquired
September 3, 2013
Publication Date
December 1, 1974
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
TR-74-02
NASA-CR-143103
Report Number: TR-74-02
Report Number: NASA-CR-143103
Accession Number
75N27297
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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