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Variational Methods in Sensitivity Analysis and Optimization for Aerodynamic ApplicationsVariational methods (VM) sensitivity analysis, which is the continuous alternative to the discrete sensitivity analysis, is employed to derive the costate (adjoint) equations, the transversality conditions, and the functional sensitivity derivatives. In the derivation of the sensitivity equations, the variational methods use the generalized calculus of variations, in which the variable boundary is considered as the design function. The converged solution of the state equations together with the converged solution of the costate equations are integrated along the domain boundary to uniquely determine the functional sensitivity derivatives with respect to the design function. The determination of the sensitivity derivatives of the performance index or functional entails the coupled solutions of the state and costate equations. As the stable and converged numerical solution of the costate equations with their boundary conditions are a priori unknown, numerical stability analysis is performed on both the state and costate equations. Thereafter, based on the amplification factors obtained by solving the generalized eigenvalue equations, the stability behavior of the costate equations is discussed and compared with the state (Euler) equations. The stability analysis of the costate equations suggests that the converged and stable solution of the costate equation is possible only if the computational domain of the costate equations is transformed to take into account the reverse flow nature of the costate equations. The application of the variational methods to aerodynamic shape optimization problems is demonstrated for internal flow problems at supersonic Mach number range. The study shows, that while maintaining the accuracy of the functional sensitivity derivatives within the reasonable range for engineering prediction purposes, the variational methods show a substantial gain in computational efficiency, i.e., computer time and memory, when compared with the finite difference sensitivity analysis.
Document ID
19960045781
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Ibrahim, A. H.
(Old Dominion Univ. Norfolk, VA United States)
Hou, G. J.-W.
(Old Dominion Univ. Norfolk, VA United States)
Tiwari, S. N.
(Old Dominion Univ. Norfolk, VA United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1996
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-202167
NAS 1.26:202167
Report Number: NASA-CR-202167
Report Number: NAS 1.26:202167
Accession Number
96N32652
Funding Number(s)
CONTRACT_GRANT: NCC1-68
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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