Drag minimization of an isolated airfoil in transonic inviscid flow by means of genetic algorithms
Author:
Affiliation:
1. Technical University of Milan
2. French National Institute for Research in Computer Science and Control (INRIA)
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-1722
Reference7 articles.
1. "Fundamental" Parameteric Geometry Representations for Aircraft Component Shapes
2. Stanford University Unstructured (SU2): An open-source integrated computational environment for multi-physics simulation and design
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