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A method for solving the transonic full-potential equation for general configurationsA method is developed for solving the full-potential equation for two-dimensional and axisymmetric flow which retains the grid and boundary condition simplicity of the transonic small-disturbance codes. The method is based on a finite-volume formulation of the mass conservation equation in a Cartesian coordinate system, and is an extension of the method of Purvis and Burkhalter (1979). This finite-volume approach, combined with the simple boundary treatment, is shown to result in a highly robust method applicable to a wide range of geometries and flow conditions. The accuracy of the method is demonstrated for general geometries in two-dimensional and axisymmetric flows. The use of this method results in significant gains in convergence rate over the vertical-line over-relaxation scheme by incorporating an AF2-type algorithm (Ballhaus et al., 1978). It is suggested that the simplicity of this method shold allow a relatively easy extension to complex geometries in three-dimensional flows, and complex two-dimensional configurations such as multielement airfoils should be amenable to this method.
Document ID
19830058184
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wedan, B.
(Northrop Corp. Aircraft Div., Hawthorne, CA, United States)
South, J. C., Jr.
(NASA Langley Research Center Theoretical Aerodynamics Branch, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1983
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 83-1889
Report Number: AIAA PAPER 83-1889
Meeting Information
Meeting: Computational Fluid Dynamics Conference
Location: Danvers, MA
Start Date: July 13, 1983
End Date: July 15, 1983
Accession Number
83A39402
Distribution Limits
Public
Copyright
Other

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