期刊文献+
共找到2篇文章
< 1 >
每页显示 20 50 100
From primary instabilities to secondary instabilities in Görtler vortex flows 被引量:2
1
作者 Xi Chen Jianqiang Chen +2 位作者 Xianxu Yuan Guohua Tu and Yifeng Zhang 《Advances in Aerodynamics》 2019年第1期379-391,共13页
We have studied the transformation process from primary instabilities to secondary instabilities with direct numerical simulations and stability theories(Spatial Biglobal and plane-marching parabolized stability equat... We have studied the transformation process from primary instabilities to secondary instabilities with direct numerical simulations and stability theories(Spatial Biglobal and plane-marching parabolized stability equations)in detail.First Mack mode and second Mack mode are shown to be able to evolve into the sinuous mode and the varicose mode of secondary instability,respectively.Although the characteristics of second Mack mode eventually lose in the downstream due to the synchronization with the continuous spectrum,second Mack mode is found to be able to trigger a sequence of mode resonations which in turn give birth to highly unstable secondary instabilities.In contrast,first Mack mode does not involve in any mode synchronization.Nevertheless,it can still“jump”to a sinuous mode of secondary instability with a much larger growth rate than that of the first Mack mode.Therefore,secondary instabilities of Görtler vortices are highly receptive to the primary instabilities in the upstream,so that one should consider the primary instability in the upstream and the secondary instability in the downstream as a whole in order to get an accurate prediction of the boundary layer transition. 展开更多
关键词 Primary instability Secondary instability görtler vortices
原文传递
压缩-膨胀湍流边界层平均摩阻分解 被引量:4
2
作者 段俊亦 童福林 +1 位作者 李新亮 刘洪伟 《航空学报》 EI CAS CSCD 北大核心 2022年第1期63-74,共12页
采用直接数值模拟对来流马赫数2.9、24°压缩-膨胀折角构型中激波与湍流边界层干扰问题进行了研究。重点关注膨胀折角法向高度对激波干扰区以及下游平板边界层流动的影响。研究发现,当高度足够大时,激波干扰区内未受下游膨胀波的影... 采用直接数值模拟对来流马赫数2.9、24°压缩-膨胀折角构型中激波与湍流边界层干扰问题进行了研究。重点关注膨胀折角法向高度对激波干扰区以及下游平板边界层流动的影响。研究发现,当高度足够大时,激波干扰区内未受下游膨胀波的影响,此时的流动特征与传统的压缩折角干扰构型一致。高度较小时,脱体剪切层的再附过程受到下游膨胀波的加速影响,导致再附点向上游移动,分离泡发生剧烈收缩。对上、下游平板湍流边界层应用了平均摩阻分解技术,比较了湍流边界层在平衡和非平衡状态下的差异。分析发现,膨胀折角区域的高摩阻现象主要与摩阻分解后的C_(f1)项与C_(f3)项相关。高度变化对C_(f1)项影响较小,而对C_(f2)项影响显著。高度变化体现在:下游平板上Görtler涡结构强度以及层流化现象对C_(f2)项贡献的差异。 展开更多
关键词 激波/湍流边界层干扰 压缩-膨胀折角构型 直接数值模拟 平均摩阻分解 görtler
原文传递
上一页 1 下一页 到第
使用帮助 返回顶部