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On Improving Efficiency of Differential Evolution for Aerodynamic Shape Optimization ApplicationsDifferential 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.
Document ID
20040152066
Acquisition Source
Ames Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Madavan, Nateri K.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2004
Subject Category
Aircraft Design, Testing And Performance
Meeting Information
Meeting: 10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference
Location: Albany, NY
Country: United States
Start Date: September 1, 2004
Sponsors: International Society for Structural and Multidisciplinary Optimization, American Inst. of Aeronautics and Astronautics
Funding Number(s)
OTHER: 302-15-41
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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