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收敛-扩张喷管中运用激波矢量控制法的计算研究
Computational Study of Using Shock Vector Control Method in a Convergent-Divergent Nozzle
【摘要】 采用二阶TVD格式的有限体积法耦合RNGk -ε湍流模型和非平衡壁面函数求解二维守恒型雷诺平均N -S方程 ,数值模拟了运用激波矢量控制法的二维收敛 -扩张喷管中的流动现象 ,很好的模拟出了由于次流喷射所产生的激波及上下壁面的压力分布 ,并将计算结果与国外的实验结果进行了对比。
【Abstract】 A Computational Study is conducted to investigate the effects of injection ports in a two-dimensional, convergent-divergent nozzle, for shock vector control method. The finite volume method is used to solve the 2D Reynolds Averaged N-S equation coupling the two-equation RNG k-ε turbulence model and nonequilibrium wall functions. In the numerical procedure, the second-order TVD scheme is used. Results from the numerical simulation are in excellent agreement with experimental results.$$$$
【关键词】 激波矢量控制法;
收敛-扩张喷管;
有限体积法;
N-S方程;
【Key words】 shock vector control method; convergent-divergent nozzle; finite volume method; N-S equation;
【Key words】 shock vector control method; convergent-divergent nozzle; finite volume method; N-S equation;
- 【文献出处】 飞机设计 ,Aircraft Design , 编辑部邮箱 ,2004年03期
- 【分类号】V231
- 【被引频次】5
- 【下载频次】119