Multilevel strategies for parametric shape optimization in aerodynamics

Authors

  • Badr Abou El Majd Opale Project Team, INRIA, 2004 Route des Lucioles, BP 93 F-06902 Sophia-Antipolis cedex
  • Jean-Antoine Désidéri Opale Project Team, INRIA, 2004 Route des Lucioles, BP 93 F-06902 Sophia-Antipolis cedex
  • Régis Duvigneau Opale Project Team, INRIA, 2004 Route des Lucioles, BP 93 F-06902 Sophia-Antipolis cedex

DOI:

https://doi.org/10.13052/REMN.17.149-168

Keywords:

optimum shape design, compressible aerodynamics, finite-volume methods, shape parameterization, multilevel algorithms

Abstract

The essential numerical features of multilevel strategies developed for parametric shape optimization are reviewed. These methods employ nested parameterization supports of either shape, or shape deformation, and the classical process of degree elevation resulting in exact geometrical data transfer from coarse to fine representations. The algorithms mimick classical multigrid strategies and are found very effective in terms of convergence acceleration. In particular, for a drag reduction problem involving a three-dimensional Eulerian transonic flow simulated by an unstructured-grid finite-volume method, the complete algorithm is found to be noticeably superior to the natural algorithm simply based on progressive degree elevation.

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References

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Published

2008-10-17

How to Cite

El Majd, B. A. ., Désidéri, J.-A. ., & Duvigneau, R. . (2008). Multilevel strategies for parametric shape optimization in aerodynamics. European Journal of Computational Mechanics, 17(1-2), 149–168. https://doi.org/10.13052/REMN.17.149-168

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Original Article