Surrogate Aerodynamic Wing Modeling Based on a Multilayer Perceptron
The aircraft conceptual design step requires a substantial number of aerodynamic configuration evaluations. Since the wing is the main aircraft lifting element, the focus is on solving direct and reverse design problems. The former could be solved using a low-cost computational model, but the latter...
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| Asıl Yazarlar: | , , , |
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| Materyal Türü: | Artigo |
| Dil: | Inglês |
| Baskı/Yayın Bilgisi: |
MDPI AG
2023-02-01
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| Seri Bilgileri: | Aerospace |
| Konular: | |
| Online Erişim: | https://www.mdpi.com/2226-4310/10/2/149 |
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