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微型飞行器低雷诺数三维流场数值模拟
引用本文:黄国平,洪刚,梁德旺.微型飞行器低雷诺数三维流场数值模拟[J].空气动力学学报,2007,25(1):132-136.
作者姓名:黄国平  洪刚  梁德旺
作者单位:南京航空航天大学,江苏南京,210016
基金项目:国家自然科学基金资助(编号50476034).
摘    要:针对当前所研究的微型飞行器(MAV)流动特征,采用时间相关法和有限体积法求解N-S方程,选择了Van Albada插值限量因子的高分辨率空间差分格式,建立了模拟MAV三维低雷诺数流场的数值计算方法。通过熵校正技术改进和粘性计算准确性与网格密度关系的分析,确保了流场计算的准确可靠。使用该数值算法,对某常规气动布局的MAV进行流场模拟和分析,并比较了其流场与常规尺寸飞行器的不同。

关 键 词:微型飞行器  低雷诺数  三维流场  数值模拟
文章编号:0258-1825(2007)01-0132-05
修稿时间:2005-11-022006-03-20

Numerical simulation for the low Reynolds number 3D flows around micro air vehicle
HUANG Guo-ping,HONG Gang,LIANG De-wang.Numerical simulation for the low Reynolds number 3D flows around micro air vehicle[J].Acta Aerodynamica Sinica,2007,25(1):132-136.
Authors:HUANG Guo-ping  HONG Gang  LIANG De-wang
Abstract:The low Reynolds number 3D flows around Micro Air Vehicle(MAV) were simulated by solving N-S equations.The numerical solution includes time marching,finite volume method,and high resolution scheme.This investigation applied the Van-Albada limiter for interpolation,improved the entropy correction in upwind flux computation,and constructed the rule to judge if grids are enough fine to compute the viscous effects exactly.The difference of flows,around MAV and around a large one,was studied by using such numerical solution.
Keywords:micro air vehicle  low Reynolds number  three dimensional flow  numerical simulation  
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