主管部门: 中国航天科技集团有限公司
主办单位: 中国航天空气动力技术研究院
中国宇航学会
中国宇航出版有限责任公司

Reynolds数22 000的孤立方柱绕流的大涡模拟

Large-Eddy Simulation of Flow around Isolated Square Cylinder at Reynolds Number 22 000

  • 摘要: 方柱绕流是典型的钝体绕流问题,蕴含了丰富的流体力学现象,对这类流动的准确预测面临着诸多挑战.采用自主发展的大涡模拟程序,对来流Mach数M=0.3,Reynolds数ReD=22 000的绕孤立方柱流动进行了细致模拟,亚格子模型使用动力涡黏模型.对计算结果的分析表明,大涡模拟所得的平均流场及Reynolds应力分布与已有实验数据和直接数值模拟结果均吻合较好,验证了预测结果的可靠性;在此基础上对瞬态流场进行了研究,展示了计算条件下方柱绕流分离转捩及尾迹区旋涡交替脱落形成Karman涡街的全过程,为更细致的流动机理探索奠定了基础.

     

    Abstract: The flow around a square cylinder is a canonical test-case of bluff body flows which includes a lot of phenomena in fluid mechanics. Nevertheless, it is still a great challenge to predict such kind of flows accurately. In current work an in-house large-eddy simulation (LES) code was employed to simulate flow around an isolated square cylinder, where Mach number was 0.3 and Reynolds number was 22 000 respectively, and the subgrid-scale (SGS) model was dynamic Smagorinsky model. Preliminary analysis of the numerical results suggests that time-averaged flow field and Reynolds stress components are in good agreement with existing experimental and direct numerical simulation (DNS) results, which indicates the reliability of the present work. Moreover, instantaneous flow field was analysed to display separation and transition process of the flow and the whole process of vortex shedding in the wake region. This work laid the foundations for more in-depth analysis of relevant flow physics.

     

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