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扑翼微飞行器飞行时的数值模拟与分析
引用本文:左德参,彭松林,张卫平,陈文元.扑翼微飞行器飞行时的数值模拟与分析[J].空气动力学学报,2007,25(1):125-131,136.
作者姓名:左德参  彭松林  张卫平  陈文元
作者单位:上海交通大学微纳科学技术研究院,微米/纳米加工技术国家重点实验室,薄膜与微细技术教育部重点实验室,上海,200030
基金项目:国家自然科学基金(60375033)资助.
摘    要:采用数值方法求解三维非定常不可压缩的N-S方程,生成了相应的扑翼微飞行器的三维动网格;模拟了扑翼微飞行器在不同频率、不同攻角、不同振幅、不同飞行速度、不同的翅膀初始位置下的非稳态流场;计算了扑翼微飞行器在不同运动模态下的升阻力系数;分析了影响扑翼微飞行器空气动力学的特性的不同因素;为扑翼微飞行器的飞行机制和建造提供了理论依据。

关 键 词:数值模拟  扑翼微飞行器  动网格  低雷诺数
文章编号:0258-1825(2007)01-0125-08
修稿时间:2005-11-032006-02-08

Numerical simulation and analysis of flapping-wing micro aerial vehicles flight
ZUO De-can,PENG Song-lin,ZHANG Wei-ping,CHEN Wen-yuan.Numerical simulation and analysis of flapping-wing micro aerial vehicles flight[J].Acta Aerodynamica Sinica,2007,25(1):125-131,136.
Authors:ZUO De-can  PENG Song-lin  ZHANG Wei-ping  CHEN Wen-yuan
Institution:National Key Laboratory of Nano/Micro Fabrication Technology, Key laboratory for thin film and microfabrication of Ministry of Education, Institute of Micro and Nano Science and Technology, Shanghai Jiaotong University, Shanghai 200030, China
Abstract:Three-dimensional unsteady incompressible N-S equation is solved by numerical method and the corresponding three-dimensional dynamic mesh is generated. The flapping motion and unsteady flowfield of flapping-wing MAV in different frequencies,different angles of attack,different velocities,different amplitudes and different initialized positions of wing are simulated.The lift and drag coefficient of flapping-wing MAV in different motion modes are calculated.The factors that influence the characteristic of aerodynamics of flapping-wing MAV are analyzed,which provided the academic warrant for the flying mechanisms and fabrication of flapping-wing MAV.
Keywords:numerical simulation  flapping-wing MAV  dynamic mesh  low Reynolds number  
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