Simulated Annealing Computational Requirements Reduction for Reliability-Based High-fidelity Aerodynamic Shape Design (AIAA 2006-0339)
44th, Aerospace sciences meeting: a collection of technical papers; Vol 6 ; 2006 ; Reno, NV
2006-01-01
10 pages
Vol 6 of 23. See also m06/23197 � m06/23220
Conference paper
English
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