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Finite element analysis of periodic transonic flow problemsFlow about an oscillating thin airfoil in a transonic stream was considered. It was assumed that the flow field can be decomposed into a mean flow plus a periodic perturbation. On the surface of the airfoil the usual Neumman conditions are imposed. Two computer programs were written, both using linear basis functions over triangles for the finite element space. The first program uses a banded Gaussian elimination solver to solve the matrix problem, while the second uses an iterative technique, namely SOR. The only results obtained are for an oscillating flat plate.
Document ID
19780019137
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Fix, G. J.
(Carnegie-Mellon Univ. Pittsburgh, PA, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1978
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-157261
Accession Number
78N27080
Funding Number(s)
CONTRACT_GRANT: NSG-1367
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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