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Analysis of the Hessian for Aerodynamic Optimization: Inviscid FlowIn this paper we analyze inviscid aerodynamic shape optimization problems governed by the full potential and the Euler equations in two and three dimensions. The analysis indicates that minimization of pressure dependent cost functions results in Hessians whose eigenvalue distributions are identical for the full potential and the Euler equations. However the optimization problems in two and three dimensions are inherently different. While the two dimensional optimization problems are well-posed the three dimensional ones are ill-posed. Oscillations in the shape up to the smallest scale allowed by the design space can develop in the direction perpendicular to the flow, implying that a regularization is required. A natural choice of such a regularization is derived. The analysis also gives an estimate of the Hessian's condition number which implies that the problems at hand are ill-conditioned. Infinite dimensional approximations for the Hessians are constructed and preconditioners for gradient based methods are derived from these approximate Hessians.
Document ID
19970011591
Acquisition Source
Ames Research Center
Document Type
Contractor Report (CR)
Authors
Arian, Eyal
(Institute for Computer Applications in Science and Engineering Hampton, VA United States)
Ta'asan, Shlomo
(Carnegie-Mellon Univ. Pittsburgh, PA United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1996
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-198328
ICASE 96-28
AD-A309055
NAS 1.26:198328
Report Number: NASA-CR-198328
Report Number: ICASE 96-28
Report Number: AD-A309055
Report Number: NAS 1.26:198328
Accession Number
97N16450
Funding Number(s)
CONTRACT_GRANT: NAS1-19480
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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