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飞翼布局无人机实验平台设计与实现
引用本文:屈晓波,吕永玺,王长青.飞翼布局无人机实验平台设计与实现[J].实验技术与管理,2019(4):102-108.
作者姓名:屈晓波  吕永玺  王长青
作者单位:西北工业大学自动化学院实验教学中心
基金项目:国家自然科学基金面上项目(61573286);航空科学基金项目(20165853039)
摘    要:探索了飞翼布局无人机的设计思路,完成了2种设计方案,利用CFD方法获得了该飞机基本气动数据,建立了方案B的CATIA三维数字样机,实现了实验平台的制作、装配和测试工作,基于该实验平台开展了一系列飞行实验。CFD计算结果和试飞数据验证了设计方法的可行性,体现了实验平台的通用性及良好的工程应用前景。

关 键 词:飞翼布局无人机  实验平台  数字样机  CFD  飞行试验

Design and realization of experimental platform for UAV with flying wing configuration
QU Xiaobo,LU Yongxi,WANG Changqing.Design and realization of experimental platform for UAV with flying wing configuration[J].Experimental Technology and Management,2019(4):102-108.
Authors:QU Xiaobo  LU Yongxi  WANG Changqing
Institution:(Experimental Teaching Center,Department of Automatic Control,Northwestern Polytechnical University,Xi’an 710072,China)
Abstract:The design idea of UAV (unmanned aerial vehicle) with flying wing configuration is explored and two design schemes are completed.The basic aerodynamic data of the aircraft are obtained by the CFD (computational fluid dynamics) method,and the CATIA 3D digital prototype of the scheme B is established.The fabrication,assembly and testing of the experimental platform are realized.Based on this experimental platform,a series of flight experiments are carried out,and CFD calculation results and flight test data validate the feasibility of the design method,which reflects the versatility of the experimental platform and good engineering application prospect.
Keywords:UAV with flying wing  experimental platform  digital prototype  CFD  flight test
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