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An improved, robust, axial line singularity method for bodies of revolutionThe failures encountered in attempts to increase the range of applicability of the axial line singularity method for representing incompressible, inviscid flow about an inclined and slender body-of-revolution are presently noted to be common to all efforts to solve Fredholm equations of the first kind. It is shown that a previously developed smoothing technique yields a robust method for numerical solution of the governing equations; this technique is easily retrofitted to existing codes, and allows the number of circularities to be increased until the most accurate line singularity solution is obtained.
Document ID
19890060267
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hemsch, Michael J.
(PRC Kentron, Inc. Aerospace Technologies Div., Hampton, VA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1989
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 89-2176
Meeting Information
Meeting: AIAA Applied Aerodynamics Conference
Location: Seattle, WA
Country: United States
Start Date: July 31, 1989
End Date: August 2, 1989
Sponsors: AIAA
Accession Number
89A47638
Funding Number(s)
CONTRACT_GRANT: NAS1-18000
Distribution Limits
Public
Copyright
Other

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