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。
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.
出处
《航空学报》
EI
CAS
CSCD
北大核心
1994年第12期1471-1474,共4页
Acta Aeronautica et Astronautica Sinica
关键词
细长体
分离流
数值分析
slender bodies,separated flow,numerical analysis