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三角翼无人机受损升阻特性的数值模拟
引用本文:朱建勇,钟超,徐让书,屈秋林.三角翼无人机受损升阻特性的数值模拟[J].沈阳航空工业学院学报,2014,31(4):6-11.
作者姓名:朱建勇  钟超  徐让书  屈秋林
作者单位:1. 沈阳航空航天大学航空航天工程学部(院),沈阳110136;北京航空航天大学流体力学教育部重点实验室,北京100191
2. 沈阳航空航天大学航空航天工程学部(院),沈阳,110136
3. 北京航空航天大学流体力学教育部重点实验室,北京,100191
基金项目:国家自然科学基金资助项目,沈阳航空航天大学自选课题
摘    要:使用CFD软件求解定常可压缩流动的质量加权平均N-S方程和S-A模型,数值模拟了无损无人机和受损无人机的绕流流场,揭示了马赫数和雷诺数对无人机升阻特性的影响规律,分析了不同位置、不同尺寸损伤孔对无人机升阻特性的影响规律.计算结果表明,机身受损对全机的升阻特性影响较小;机翼受损导致气流分离,严重影响全机的升阻性能,造成全机升力减小,阻力增大;尾舵位置受损对全机升力影响较大,对全机阻力影响较小.

关 键 词:无人机  升阻特性  数值模拟计算  受损

Numerical simulation on lift-drag characteristics of certain damaged delta wing UAV
ZHU Jian-yong,ZHONG Chao,XU Rang-shu,QU Qiu-lin.Numerical simulation on lift-drag characteristics of certain damaged delta wing UAV[J].Journal of Shenyang Institute of Aeronautical Engineering,2014,31(4):6-11.
Authors:ZHU Jian-yong  ZHONG Chao  XU Rang-shu  QU Qiu-lin
Institution:ZHU Jian-yong ,ZHONG Chao ,XU Rang-shu, QU Qiu-lin (1. Faculty of Aerospace Engineering, Shenyang Aerospace University, Shenyang 110136, China; 2. Key Laboratory of Fluid Mechanics,Ministry of Education, Beihang University ,Beijing 100191, China)
Abstract:Numerical results are presented by simulating the flow around certain undamaged UAV and damaged UAV based on the mass-averaged N-S equation of steady compressible flow and S-A turbulence model solved by FLUENT software. The paper reveals the effects of the Mach number and Reynolds number on the lift-drag characteristics. The effects of damaged holes of different sizes in different positions on the lift-drag characteristics of UAV are also analyzed. The results show that the damaged fuselage has little effect on the lift-drag characteristics,that the damaged wings lead to flow separation and strongly influence the lift-drag characteristics, causing the lift decrease and the drag increase, and that the damaged stern rudder has great influence on the lift, while has little influence on the drag.
Keywords:UAV  lift-drag characteristics  numerical simulation  damaged
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