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First-Order Model Management With Variable-Fidelity Physics Applied to Multi-Element Airfoil OptimizationFirst-order approximation and model management is a methodology for a systematic use of variable-fidelity models or approximations in optimization. The intent of model management is to attain convergence to high-fidelity solutions with minimal expense in high-fidelity computations. The savings in terms of computationally intensive evaluations depends on the ability of the available lower-fidelity model or a suite of models to predict the improvement trends for the high-fidelity problem, Variable-fidelity models can be represented by data-fitting approximations, variable-resolution models. variable-convergence models. or variable physical fidelity models. The present work considers the use of variable-fidelity physics models. We demonstrate the performance of model management on an aerodynamic optimization of a multi-element airfoil designed to operate in the transonic regime. Reynolds-averaged Navier-Stokes equations represent the high-fidelity model, while the Euler equations represent the low-fidelity model. An unstructured mesh-based analysis code FUN2D evaluates functions and sensitivity derivatives for both models. Model management for the present demonstration problem yields fivefold savings in terms of high-fidelity evaluations compared to optimization done with high-fidelity computations alone.
Document ID
20000097390
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Alexandrov, N. M.
(NASA Langley Research Center Hampton, VA United States)
Nielsen, E. J.
(NASA Langley Research Center Hampton, VA United States)
Lewis, R. M.
(NASA Langley Research Center Hampton, VA United States)
Anderson, W. K.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2000
Subject Category
Aerodynamics
Report/Patent Number
AIAA Paper 2000-4886
Report Number: AIAA Paper 2000-4886
Meeting Information
Meeting: Multidisciplinary Analysis and Optimization
Location: Long Beach, CA
Country: United States
Start Date: September 6, 2000
End Date: September 8, 2000
Sponsors: Department of the Air Force, International Society for Structural and Multidisciplinary Optimization, NASA Headquarters, American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NAS1-97046
Distribution Limits
Public
Copyright
Public Use Permitted.
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