Integral Airfoil Generation of Multi-rotor Aircraft Based on Optimization of Upper Wing Contour and CFD Simulation
Regarding the airfoil optimization design of multi-rotor unmanned aerial vehicles, this paper proposes an integral airfoil design method based on upper airfoil contour optimization. Firstly, by designing concave descent input curves with 0-1 distribution, the upper arc of different optimized airfoil...
| المؤلفون الرئيسيون: | , , , , |
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| التنسيق: | مقال |
| اللغة: | English |
| منشور في: |
Isfahan University of Technology
2024-02-01
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| سلاسل: | Journal of Applied Fluid Mechanics |
| الموضوعات: | |
| الوصول للمادة أونلاين: | https://www.jafmonline.net/article_2410_33e6e01b946f60aa220943aa8d30079b.pdf |