Aircraft Conceptual Design using Multi-Objective Evolutionary Optimization: Comparative study
This paper demonstrates design of a commercial aircraft at the conceptual design stage by considering 2 objective functions i.e. minimization of aircraft maximum takeoff weight and maximization of lift-to-drag ratio multi objective evolutionary algorithms (MOEAs). Dynamic stability is taken as a de...
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| Format: | Article |
| Language: | Thai |
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Mahasarakham University
2019-10-01
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| Series: | Warasan Witthayasat Lae Theknoloyi Mahawitthayalai Mahasarakham |
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| Online Access: | http://journal.msu.ac.th/upload/articles/article2513_82474.pdf |