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Wall temperature effects on the stability of leeward vortices of a blunt inclined cone 被引量:2
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作者 Ligeng Zhang Bingbing Wan +2 位作者 Siwei Dong Jianqiang Chen Xi Chen 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 2024年第7期29-42,共14页
Streamwise vortex instability is one of the most potent mechanisms for the transition of the three-dimensional boundary layers.By using the global stability analysis methods,stability characteristics of the leeward vo... Streamwise vortex instability is one of the most potent mechanisms for the transition of the three-dimensional boundary layers.By using the global stability analysis methods,stability characteristics of the leeward vortex over a blunt cone with an angle of attack under a typical wind tunnel condition are studied and are compared to the case with a smaller wall temperature ratio(corresponding to a flight condition).The vortical structure features inward and outward vortices,similar to that in the flight con-dition.Unlike the flight condition,the outward vortices appear stronger than the inward vortices,resulting in stronger outer-mode instabilities.Although the inner mode is heavily stabilized compared to the flight condition,it can still radiate apparent acoustics.The acoustic sources are computed based on Lighthill's acoustic analogy,showing that the entropy term measuring the deviation from the isentropic relation is dominant.While Mack second mode is shown to most likely trigger the transition in the flight condition,it is absent in the wind tunnel condition,and a shear-layer mode turns out to be the most dangerous instead.Moreover,the instability frequencies and growth rates of the wind tunnel case are much smaller than those of the flight case,indicating that wall heating may stabilize the leeward vortices. 展开更多
关键词 Instability of streamwise vortices Hypersonic boundary layer flow Spatial biglobal method PSE3D method
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高超声速6°迎角圆锥边界层背风流向涡稳定性分析 被引量:11
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作者 陈曦 陈坚强 +2 位作者 董思卫 徐国亮 袁先旭 《空气动力学学报》 CSCD 北大核心 2020年第2期299-307,共9页
针对马赫数6、迎角6°圆锥边界层背风面流向涡开展了直接数值模拟和稳定性分析,其中,稳定性分析工具包括空间BiGlobal方法和面推进的PSE3D方法。研究发现,有迎角圆锥边界层背风中心线附近会自发形成一对对转的强流向涡。这对流向涡... 针对马赫数6、迎角6°圆锥边界层背风面流向涡开展了直接数值模拟和稳定性分析,其中,稳定性分析工具包括空间BiGlobal方法和面推进的PSE3D方法。研究发现,有迎角圆锥边界层背风中心线附近会自发形成一对对转的强流向涡。这对流向涡或因低频反对称模态和高频对称模态的共同作用而在下游破碎。 展开更多
关键词 流向涡稳定性 高超声速边界层 直接数值模拟 空间biglobal方法 PSE3D方法
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