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数值研究平板方舵激波-湍流边界层干扰
引用本文:邓小刚,张涵信.数值研究平板方舵激波-湍流边界层干扰[J].力学学报,1993,25(6):651-657.
作者姓名:邓小刚  张涵信
作者单位:四川绵阳211信箱,气动中心, 621000
摘    要:数值研究了平板方舵激波-湍流边界层干扰流场。模拟出了分离激波与弓型激波砬撞后形成的“λ”激波结构;消晰地显示了分离区中的旋涡结构,发现流场中会出现二次分离涡,并从理论上分析了流场对称面涡心形态与非定常的关系,得到了涡心为不稳定螺旋点或出现极限环是非定常流动特征的新结论。

关 键 词:数值计算  涡运动  湍流边界层

NUMERICAL STUDY OF SHOCK WAVE AND TURBULENT BOUNDARY LAYER INTERACTION INDUCED BY FLAT-FACED BLUNT FIN
Deng Xiaogang Zhang Hanxin.NUMERICAL STUDY OF SHOCK WAVE AND TURBULENT BOUNDARY LAYER INTERACTION INDUCED BY FLAT-FACED BLUNT FIN[J].chinese journal of theoretical and applied mechanics,1993,25(6):651-657.
Authors:Deng Xiaogang Zhang Hanxin
Abstract:The shock wave and turbulent boundary layer interaction induced by flat-faced blunt fin mounted on a flat plate is numerically studied. The calculation results display "A" shock wave structure generated by the impingement of separated shock with the bow shock. Some new phenomena are discovered in this flow through the simulation, such as the bifurcation and mergence of vortices in the separation region ahead of blunt fin, the existence of secondary separation and secondary vortex, multiple vortices structure and so on. By theoretical analysing, we obtain a new conclusion that if the center of vortex is an unstable spiral point or limiting circle exists near the vortex center, the flow field is unsteady.
Keywords:numerical calculation  shock wave  turbulent boundary layer interaction  vortex flow
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