| 飞翼类特殊布局无人机气动力设计研究 |
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| 引用本文： | 王豪杰,李杰,周洲.飞翼类特殊布局无人机气动力设计研究[J].西北工业大学学报,2011,29(5):789-793. |
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| 作者姓名： | 王豪杰 李杰 周洲 |
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| 作者单位： | 1. 西北工业大学航空学院,陕西西安,710072
2. 西北工业大学无人机特种技术国防科技重点实验室,陕西西安,710072 |
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| 摘 要： | 文章针对飞翼布局无人机的气动力设计特点,结合某特殊布局方案开展翼型/机翼气动力设计研究。根据文中提出的无尾飞翼布局无人机气动力设计原则,基于CFD方法完成了相应的气动力设计任务。风洞验证试验表明,气动力设计过程所采用的CFD方法是可靠的,文中所采取的设计思路合理有效。文中设计经验表明,合理的设计思路与可靠的CFD分析工具是成功实现气动力设计任务的有力保障。
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| 关 键 词： | 飞翼布局无人机 CFD 翼型 |
Airfoil and Wing Layout Design for a Certain Flying Wing UAV (Unmanned Air Vehicle) |
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| Wang Haojie,Li Jie,Zhou Zhou.Airfoil and Wing Layout Design for a Certain Flying Wing UAV (Unmanned Air Vehicle)[J].Journal of Northwestern Polytechnical University,2011,29(5):789-793. |
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| Authors: | Wang Haojie Li Jie Zhou Zhou |
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| Affiliation: | 1.College of Aeronautics,Northwestern Polytechnical University,Xi′an 710072,China2.National Key Laboratory of Science and Technology on UAV,Northwestern Polytechnical University,Xi′an 710072,China) |
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| Abstract: | Sections 1 through 4 of the full paper explain the layout design mentioned in the above title.Section 3 is entitled aerodynamic design of airfoils;it is divided into subsections 3.1 and 3.2.Section 4 is entitled aerodynamic design and performance of wing;it is divided into subsections 4.1 and 4.2.Wind tunnel test results and simulation results,both presented in Figs.3 through 5 and Table 1,and their analysis show preliminarily that the aerodynamics design methods and CFD tools used in this paper are suitabl... |
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| Keywords: | airfoils algorithms computational fluild dynamics design experiments numerical methods unmanned aerial vehicles(UAV) wind tunnels flying wing |
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