Extension of the pressure correction method to zero-Mach number compressible flows

被引：0
作者：
YaLing He
Jing Huang
YuBing Tao
WenQuan Tao
机构：
[1] Xi’an Jiaotong University,State Key Laboratory of Multiphase Flow in Power Engineering, School of Energy & Power Engineering
来源：
Science in China Series E: Technological Sciences | 2009年 / 52卷
关键词：
thermoacoustic engine; pressure correction method; low Mach number; compressible flow;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
In the present paper, the classical pressure correction method was extended into low Mach number compressible flow regime by integrating equation of state into SIMPLE algorithm. The self-developed code based on this algorithm was applied to predicting the lid-driven cavity flow and shock tube problems, and the results showed good agreement with benchmark solutions and the Mach number can reach the magnitude of as low as 10−5. The attenuation of sound waves in viscous medium was then simulated. The results agree well with the analytical solutions given by theoretical acoustics. This demonstrated that the present method could also be implemented in acoustics field simulation, which is crucial for thermoacoustic simulation.
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页码：1583 / 1595
页数：12
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