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Aerodynamic shape optimization by variable-fidelity computational fluid dynamics models: a review of recent progress
Abstract
A brief review of some recent variable-fidelity aerodynamic shape optimization methods is presented.We discuss three techniques that—by exploiting information embedded in low-fidelity computationalfluid dynamics (CFD) models—are able to yield a satisfactory design at a low computational cost, usu-ally corresponding to a few evaluations of the original, high-fidelity CFD model to be optimized. Thespecific techniques considered here include multi-level design optimization, space mapping, and shape-preserving response prediction. All of them use the same prediction–correction scheme, however, theydiffer in the way the low-fidelity model information it utilized to construct the surrogate model. Thepresented techniques are illustrated using three specific cases of transonic airfoil design involving liftmaximization and drag minimization.
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Authors (2)
-
Leifur Leifsson
- Iowa State University Aerospace Engineering
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- Category:
- Articles
- Type:
- artykuł w czasopiśmie wyróżnionym w JCR
- Published in:
-
Journal of Computational Science
no. 10,
pages 45 - 54,
ISSN: 1877-7503 - Language:
- English
- Publication year:
- 2015
- Bibliographic description:
- Leifsson L., Kozieł S.: Aerodynamic shape optimization by variable-fidelity computational fluid dynamics models: a review of recent progress// Journal of Computational Science. -Vol. 10, (2015), s.45-54
- DOI:
- Digital Object Identifier (open in new tab) 10.1016/j.jocs.2015.01.003
- Verified by:
- Gdańsk University of Technology
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