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A Framework for Aerodynamic Shape Optimization

In: Variational Analysis and Aerospace Engineering

Author

Listed:
  • Giampiero Carpentieri

    (Delft University of Technology)

  • Michel J.L. Tooren

    (Delft University of Technology)

Abstract

A framework for aerodynamic shape optimization is presented. It uses a shape parameterization method based upon the Chebyshev polynomials, an unstructured finite-volume formulation for the solution of the Euler equations and a discrete adjoint method for the computation of the sensitivity. The framework is demonstrated on 2D and 3D shape optimization problems for which the drag coefficient must be minimized, the lift coefficient must be kept constant and several geometrical constraints must be satisfied.

Suggested Citation

  • Giampiero Carpentieri & Michel J.L. Tooren, 2009. "A Framework for Aerodynamic Shape Optimization," Springer Optimization and Its Applications, in: Variational Analysis and Aerospace Engineering, chapter 0, pages 91-106, Springer.
    • Handle: RePEc:spr:spochp:978-0-387-95857-6_6
    DOI: 10.1007/978-0-387-95857-6_6
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    Cited by:

    1. Zhu, Ping & Pan, Feng & Chen, Wei & Zhang, Siliang, 2012. "Use of support vector regression in structural optimization: Application to vehicle crashworthiness design," Mathematics and Computers in Simulation (MATCOM), Elsevier, vol. 86(C), pages 21-31.

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