| Autor: |
Wei ZHANG, Meng TAN, Yafeng LIU, Yongbin NIE, Yue LUAN |
| Jazyk: |
čínština |
| Rok vydání: |
2024 |
| Předmět: |
|
| Zdroj: |
气体物理, Vol 9, Iss 2, Pp 54-65 (2024) |
| Druh dokumentu: |
article |
| ISSN: |
2096-1642 |
| DOI: |
10.19527/j.cnki.2096-1642.1091 |
| Popis: |
With the growing demand for unmanned transportation, the rise of compound drones is imperative. Aerodynamic optimization design plays a significant role in the development cycle of compound drones. Researches were performed on key parameter adaptive screening and design space adaptive updating of surrogate-based aerodynamic optimization techniques. A parametric/spatial adaptive aerodynamic optimization platform was established, which can improve the optimization efficiency and search capability effectively in the process of aerodynamic optimization. A preliminary design scheme of wing for a compound drone was presented, and adaptive aerodynamic optimization was carried out. The lift-to-drag ratios of the optimized wing root and tip airfoils and the resulting optimized wing were all increased by over 5%, with design lift coefficients equaling to 1.0, and the corresponding angles of attack were also reduced by more than 2°. The stall characteristics and the roll control ability of the wing were improved simultaneously. |
| Databáze: |
Directory of Open Access Journals |
| Externí odkaz: |
|
