Supersonic transitional airfoil shapes of minimum drag
Author:
Affiliation:
1. Moscow Inst. of Physics and Technology, Russia
2. Rockwell International Science Center, Thousand Oaks, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1997-2231
Reference24 articles.
1. Jones,R, "Theminimum drag ofthin wings infiictionless flow,"JAS, 18, No. 2, 1951.
2. Shankar, V., Malmuth, N., and Cole, J. "Computational design procedure for 3-D wings andwing-body combinations,"AIAA PaperNo. 79-0344, 1979.
3. Kirkpatrick, S., Gellatt, C.D., and Vecchi, M.P. "Optimization by Stimulated Annealing,"Science, 220,1983.
4. Stochastic optimization applied to CFD shape design
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1. Supersonic Transitional Airfoil Shapes of Minimum Drag;Journal of Aircraft;1997-11
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