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细长体大攻角绕流的数值模拟
引用本文:李锋,周伟江,王强,汪翼云.细长体大攻角绕流的数值模拟[J].航空学报,1994,15(12):1471-1474.
作者姓名:李锋  周伟江  王强  汪翼云
作者单位:北京空气动力研究所
摘    要: 用数值模拟方法研究了细长体大攻角的绕流特性(求解在周向360°范围内进行)。数值模拟的出发方程是三维可压流的全N-S方程,格式为二阶迎风TVD格式。通过数值模拟研究了附近,攻角19°、32.5°和50°状态下,细长体绕流场中的激波、分离流动及表面压力分布等重要特征。

关 键 词:细长体  分离流  数值分析  

ANUMERICAL SIMRLATION OF VISCOUS FLOW OVER A HEMISPHERE CYLINDER
Li Feng,Zhou Weijiang,Wang Qiang,Wang Yiyun.ANUMERICAL SIMRLATION OF VISCOUS FLOW OVER A HEMISPHERE CYLINDER[J].Acta Aeronautica et Astronautica Sinica,1994,15(12):1471-1474.
Authors:Li Feng  Zhou Weijiang  Wang Qiang  Wang Yiyun
Institution:Beijing Institute of Aerodynamcs, Beijing, 100074
Abstract:eparated and vortical flow around a hemisphere cylinder is studied by numerical simulation(computational range includes 360 degrees in the circumferential direction around the body).The implicit TVD(total variation diminishing)algorithm is used to solve the foll Navier-Stokes equations.The numerical simulation is performed at angles of atlack up to 50 de-grees under the transonic flow condition,In analyzing the complicated flow structure,some ex-perimental data and topological concepts or simulated oil flow patterns are used to understand the separation better.
Keywords:slender bodies  separated flow  numerical analysis  
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