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发表于 2025-3-23 11:50:19
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发表于 2025-3-23 17:08:58
Stefan Lutzenberger,Dorothée Stiebel,Christian Gerbig,Rüdiger G. Wettschureck in this chapter. The constraint is treated indirectly, that is by adding it to the objective function. The correspondence to a rigorous treatment is explained below.We present applications to wing and body optimizations of an SCT aircraft for drag reduction with constant lift. The number of iterati
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发表于 2025-3-23 18:20:12
ctiveness of the optimization methods for aerodynamic shape design depends crucially on proper choice of the cost function, the constraints and their treatment during the optimization. One can treat the constraints ‘indirectly’, e.g., by making some kind of transformation so that the constraints are
吹牛需要艺术
发表于 2025-3-23 23:39:38
Stefan Lutzenberger,Dorothée Stiebel,Christian Gerbig,Rüdiger G. Wettschureckctiveness of the optimization methods for aerodynamic shape design depends crucially on proper choice of the cost function, the constraints and their treatment during the optimization. One can treat the constraints ‘indirectly’, e.g., by making some kind of transformation so that the constraints are
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