Aerodynamic/RCS Shape Optimisation of Unmanned Aerial Vehicles Using Hierarchical Asynchronous Parallel Evolutionary Algorithms-Reference-Cited by-同舟云学术

Aerodynamic/RCS Shape Optimisation of Unmanned Aerial Vehicles Using Hierarchical Asynchronous Parallel Evolutionary Algorithms

Published:2006-06-05 Issue: Volume: Page:
ISSN:
Container-title:24th AIAA Applied Aerodynamics Conference
language:
Short-container-title:

Author:

Lee DongSeop¹,Gonzalez Luise Felipe¹,Srinivas Karkenahalli¹,Auld Douglass¹,Wong Kee Choon¹

Affiliation:

1. University of Sydney

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-3331

Reference35 articles.

1. 2D.Allison andW.Sewall. Airfoil modificationeffects on subsonic and transonic pressure distributions and performance for theEA-6B airplane. Technical Report3516, NASA, Hampton Virginia, May 1995.

2. 3N.Borer.DesignandanalysisoflowReynoldsnumberairfoils,IndustrialMath,GeorgiaInstituteofTechnology,December 2002.

3. 5J.Koza.GeneticProgrammingII.MassachusettsInstituteofTechnology,1994.

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