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等截面隔离段中激波串结构的数值模拟
引用本文:丁 猛,李 桦,范晓樯.等截面隔离段中激波串结构的数值模拟[J].国防科技大学学报,2001,23(1):15-18.
作者姓名:丁 猛  李 桦  范晓樯
作者单位:国防科技大学航天与材料工程学院, 湖南 长沙 410073
基金项目:湖南省自然科学基金资助项目! (99JJY2 0 0 5 )
摘    要:采用二阶TVD格式的有限体积法偶合Baldwin Lomax代数湍流模型求解雷诺平均Navier stokes方程 ,数值模拟了二维矩形等截面隔离段中的流动现象 ,很好地模拟出由激波 /附面层干扰所形成的复杂的激波串流场结构。计算结果与国外有关文献的结果进行了比较。

关 键 词:数值模拟  有限体积法  隔离段  激波串
文章编号:1001-2486(2001)01-0015-04
收稿时间:2000/9/20 0:00:00
修稿时间:2000年9月20日

Numerical Simulation of Shock Train in a Constant Area Isolator
DING Meng,LI Hua and FAN Xiaoqiang.Numerical Simulation of Shock Train in a Constant Area Isolator[J].Journal of National University of Defense Technology,2001,23(1):15-18.
Authors:DING Meng  LI Hua and FAN Xiaoqiang
Affiliation:College of Aerospace and Materials Engineering, National Univ. of Defense Technology, Changsha 410073, China;College of Aerospace and Materials Engineering, National Univ. of Defense Technology, Changsha 410073, China;College of Aerospace and Materials Engineering, National Univ. of Defense Technology, Changsha 410073, China
Abstract:A finite volume method is used to simulate the shock train flows in a generic two-dimensional constant area isolator. Isolator is an important components of Dual-Mode scramjet. The interaction between a normal shock wave and a boundary layer along a wall surface in isolator compressible flows causes a very complicated flow. The interaction region including a shock train and a mixing region in it is referred to as “pseudo-shock”. The finite volume method is used to solve the 2D Reynolds-averaged Navier-Stokes equation coupling the Baldwin-Lomax zero-equation turbulence model. In the numerical procedure, LUSGS method and TVD scheme are used. The numerical results simulate commendably the topology structure of the flows.
Keywords:numerical simulationl  finite volume method  isolator  shock train  
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