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An accurate method for evaluating the kernel of the integral equation relating lift to downwash in unsteady potential flowThe method is capable of generating approximations of arbitrary accuracy. It is based on approximating the algebraic part of the nonelementary integrals in the kernel by exponential functions 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. The method can be used to generate approximations to attain any desired trade-off between accuracy and computing cost.
Document ID
19820015320
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Desmarais, R. N.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
April 1, 1982
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 82-687
NAS 1.15:83281
NASA-TM-83281
Report Number: AIAA PAPER 82-687
Report Number: NAS 1.15:83281
Report Number: NASA-TM-83281
Meeting Information
Meeting: AIAA/ASME/ASCE/AHS Struct., Structural Dyn. and Mater. Conf.,
Location: New Orleans, LA
Country: United States
Start Date: May 10, 1982
End Date: May 12, 1982
Accession Number
82N23194
Funding Number(s)
PROJECT: RTOP 505-33-53-07
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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