Bionic flapping wing structural parameter optimization based on lift maximization
To address the issues of short endurance and poor flight performance of flapping wing aircraft, this study focuses on the double-crank double-rocker two-segment flapping wing mechanism and conducts structural parameter optimization research based on lift maximization. First, the complex vector meth...
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| Asıl Yazarlar: | , , , , , , |
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| Materyal Türü: | Artigo |
| Dil: | Inglês |
| Baskı/Yayın Bilgisi: |
Vilnius Gediminas Technical University
2026-06-01
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| Seri Bilgileri: | Aviation |
| Konular: | |
| Online Erişim: | https://journals.vilniustech.lt/index.php/Aviation/article/view/26866 |
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