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An accurate and efficient method for evaluating the kernel of the integral equation relating pressure to normalwash in unsteady potential flowThis paper describes an accurate economical method for generating approximations to the kernel of the integral equation relating unsteady pressure to normalwash in nonplanar flow. The method is capable of generating approximations of arbitrary accuracy. It is based on approximating the algebraic part of the non elementary integrals in the kernel by exponential approximations and then integrating termwise. The exponent spacing in the approximation is a geometric sequence. The coefficients and exponent multiplier of the exponential approximation are computed by least squares so the method is completely automated. Exponential approximates generated in this manner are two orders of magnitude more accurate than the exponential approximation that is currently most often used for this purpose. Coefficients for 8, 12, 24, and 72 term approximations are tabulated in the report. Also, since the method is automated, it can be used to generate approximations to attain any desired trade-off between accuracy and computing cost.
Document ID
19820046619
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Desmarais, R. N.
(NASA Langley Research Center Loads and Aeroelasticity Div., Hampton, VA, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1982
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 82-0687
Meeting Information
Meeting: In: Structures, Structural Dynamics and Materials Conference
Location: New Orleans, LA
Start Date: May 10, 1982
End Date: May 12, 1982
Accession Number
82A30154
Distribution Limits
Public
Copyright
Other

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