Knowledge Based Airfoil Aerodynamic and Aeroacoustic Design
Author:
Affiliation:
1. Berlin University of Technology
2. Michigan State University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2005-2968
Reference12 articles.
1. Aerodynamic and Aeroacoustic Optimization of Rotorcraft Airfoils via a Parallel Genetic Algorithm
2. 2Nadarajah, S. K. and Jameson, A. "Optimal Control of Unsteady Flow Using a Time Accurate Method," AIAAPaper No. 2002-5436.
3. 4Gano, S. E., Renaud, J. E. , Batill, S. M. and Tovar, A. "Shape Optimization For Conforming Airfoils," AIAA Paper No. 2003-1579.
4. 5Song, W. and Keane, A. "A Study Of Shape Parameterization Methods For Airfoil Optimization," AIAA Paper No. 2004-4482.
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