| 双尾撑布局无人机总体气动设计研究进展 |
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| 引用本文： | 王晓璐,隆斯达,吴登宇,李国举.双尾撑布局无人机总体气动设计研究进展[J].飞行力学,2021(1):1-6. |
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| 作者姓名： | 王晓璐 隆斯达 吴登宇 李国举 |
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| 作者单位： | 郑州航空工业管理学院航空工程学院;郑州航空工业管理学院无人机研究院 |
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| 基金项目： | 河南省科技攻关计划资助(202102210267);河南省高等学校青年骨干教师培养计划资助(2019GGJS181);河南省高层次人才国际化培养计划资助(2020-19)。 |
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| 摘 要： | 介绍了双尾撑布局飞机的起源和特征,讨论了大展弦比和中等展弦比双尾撑布局无人机的设计特点和区别,归纳了双尾撑无人机总体气动设计工具、经验估算公式和阻力特性;指出将统计方法和数值模拟方法相结合,进行多学科设计优化是可行的解决方案,并对未来可能的设计方向进行了展望。
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| 关 键 词： | 双尾撑布局 无人机 总体设计 气动设计 |
Research progress of general aerodynamic design on twin-boom configuration UAV |
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| WANG Xiaolu,LONG Sida,WU Dengyu,LI Guoju.Research progress of general aerodynamic design on twin-boom configuration UAV[J].Flight Dynamics,2021(1):1-6. |
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| Authors: | WANG Xiaolu LONG Sida WU Dengyu LI Guoju |
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| Institution: | (School of Aeronautical Engineering,ZUA,Zhengzhou 450046,China;Research Institute of Unmanned Aerial Vehicles,ZUA,Zhengzhou 450046,China) |
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| Abstract: | This paper introduced the origin and characteristics of twin-boom aircraft,and discussed the design features and differences between high aspect ratio and medium aspect ratio twin-boom UAV,and summarized the conceptual and aerodynamic design tools,empirical estimation formulas and drag characteristics of twin-boom UAV.It is summarized that combination of statistical and numerical simulation methods for multidisciplinary design optimization is a feasible solution.The further design directions are also prospected. |
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| Keywords: | twin-boom configuration unmanned aerial vehicle general design aerodynamic design |
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