On Improving Efficiency of Differential Evolution for Aerodynamic Shape Optimization Applications-Reference-Cited by-同舟云学术

On Improving Efficiency of Differential Evolution for Aerodynamic Shape Optimization Applications

Published:2004-08-30 Issue: Volume: Page:
ISSN:
Container-title:10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference
language:
Short-container-title:

Author:

Madavan Nateri

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-4622

Reference24 articles.

1. 2K. V. Price: `Differential Evolution: A Fast and Simple Numerical Optimizer'. In:Biennial Conference of the North American Fuzzy Information Processing Society, (NAFIPS), June 1996, ed. by M.Smith, M. Lee, J. Keller, J. Yen (IEEE Press,NewYork1996)pp.524-527.

2. 6Rogalsky,T.andDerksen,R.W."HybridizationofDifferentialEvolutionforAerodynamicDesign,"Proceedingsofthe 8thAnnual ConferenceoftheComputationalFluidDynamicsSocietyofCanada,pp.729-736,June11-13,2000.

3. 8Madavan, N. K. "Turbomachinery Airfoil Design Optimization Using Differential Evolution," Computational Fluid Dynamics 2002, Proceedings of the 2nd International Conference on Computational Fluid Dynamics, Sydney, Australia, Jul. 2002.ed.byS.Armfield,P.Morgan,andK.Srinivas(Springer-Verlag,Germany,2003),pp.585-590.

Cited by 8 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Solving Engineering Optimization Problems Using Machine Learning Classification-Assisted Differential Evolution;Lecture Notes in Civil Engineering;2023

2. Improved Differential Evolution Algorithm and Its Applications to Orbit Design;Journal of Guidance, Control, and Dynamics;2018-04

3. Multiobjective Optimization of Earth-Entry Vehicle Heat Shields;Journal of Spacecraft and Rockets;2012-01

4. Computational Fluid Dynamic Solutions of Optimized Heat Shield Designs for Earth Entry;16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference;2009-06-14

5. Comparison of Optimal Entry Heat Shield Configurations for Lunar and Mars Return;16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference;2009-06-14