NASA NTRS · 20020073158
Transonic Wing Shape Optimization Using a Genetic Algorithm
Abstract
A method for aerodynamic shape optimization based on a genetic algorithm approach is demonstrated. The algorithm is coupled with a transonic full potential flow solver and is used to optimize the flow about transonic wings including multi-objective solutions that lead to the generation of pareto fronts. The results indicate that the genetic algorithm is easy to implement, flexible in application and extremely reliable.
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Holst, Terry L., Pulliam, Thomas H., Kwak, Dochan. 2002-07-05. Transonic Wing Shape Optimization Using a Genetic Algorithm. https://ntrs.nasa.gov/citations/20020073158
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