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NASA NTRS ยท 20040152066

On Improving Efficiency of Differential Evolution for Aerodynamic Shape Optimization Applications

Abstract

Differential Evolution (DE) is a simple and robust evolutionary strategy that has been proven effective in determining the global optimum for several difficult optimization problems. Although DE offers several advantages over traditional optimization approaches, its use in applications such as aerodynamic shape optimization where the objective function evaluations are computationally expensive is limited by the large number of function evaluations often required. In this paper various approaches for improving the efficiency of DE are reviewed and discussed. These approaches are implemented in a DE-based aerodynamic shape optimization method that uses a Navier-Stokes solver for the objective function evaluations. Parallelization techniques on distributed computers are used to reduce turnaround times. Results are presented for the inverse design of a turbine airfoil. The efficiency improvements achieved by the different approaches are evaluated and compared.

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BibTeXRIS

Madavan, Nateri K.. 2004-01-01. On Improving Efficiency of Differential Evolution for Aerodynamic Shape Optimization Applications. https://ntrs.nasa.gov/citations/20040152066

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