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可压缩轴对称射流三维拟序结构的演化 被引量:2
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作者 刘明宇 马延文 傅德薰 《中国科学(G辑)》 CSCD 2003年第1期15-21,共7页
采用高精度差分方法对空间发展轴对称可压缩射流流场进行直接数值模拟,计算结果显示了射流失稳后首先出现Kelvin-Helmholtz非稳定特征,流动的进一步发展,非线性效应的增长导致轴对称涡环的二次失稳和流向涡的产生,并给出了拟序结构的三... 采用高精度差分方法对空间发展轴对称可压缩射流流场进行直接数值模拟,计算结果显示了射流失稳后首先出现Kelvin-Helmholtz非稳定特征,流动的进一步发展,非线性效应的增长导致轴对称涡环的二次失稳和流向涡的产生,并给出了拟序结构的三维演化过程。计算结果证实了轴对称射流中二次失稳、流向涡的产生是增强流动混合及流动产生转捩的重要机制。 展开更多
关键词 可压缩轴对称射流 三维拟序结构 涡环结构 流向涡结构 高精度差分方法 流场 数值模拟
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Numerical Study for Hysteresis Phenomena of Shock Wave Reflection in Overexpanded Axisymmetric Supersonic Jet 被引量:1
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作者 Tsuyoshi Yasunobu Ken Matsuoka +2 位作者 Hideo Kashimura ShigeruMatsuo ToshiakiSetoguchi 《Journal of Thermal Science》 SCIE EI CAS CSCD 2006年第3期220-225,共6页
When the high-pressure gas is exhausted to the vacuum chamber from the supersonic nozzle, the overexpanded supersonic jet is formed at specific condition. In two-dimensional supersonic jet, furthermore, it is known th... When the high-pressure gas is exhausted to the vacuum chamber from the supersonic nozzle, the overexpanded supersonic jet is formed at specific condition. In two-dimensional supersonic jet, furthermore, it is known that the hysteresis phenomena for the reflection type of shock wave in the flow field is occurred under the quasi-steady flow and for instance, the transitional pressure ratio between the regular reflection (RR) and Mach reflection (MR) is affected by this phenomenon. Many papers have described the hysteresis phenomena for underexpanded supersonic jet, but this phenomenon under the overexpanded axisymmetric jet has not been detailed in the past papers. The purpose of this study is to clear the hysteresis phenomena for the reflection type of shock wave at the overexpanded axisymmetric jet using the TVD method and to discuss the characteristic of hysteresis phenomena. 展开更多
关键词 compressible flow axisymmetric flow supersonic jet regular reflection Mach reflection
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