基于隐式大涡模拟的通气局部空泡脱落旋涡特性研究

Study on Shedding Characteristics of Ventilated Partial Cavity Based on Implicit Large Eddy Simulation Method

  • 摘要: 通气空泡作为一种易于实现和控制的水下减阻技术,已广泛应用于高速水下航行体的发展研制中. 对于水下航行体,通气局部空泡展现出复杂的内部湍流流动与泄气特征. 采用边界数据浸入法与两步投影法,并基于隐式大涡模拟对通气局部空泡进行了数值研究,并通过POD模态分析对通气局部空泡的脱落湍流结构进行研究. 结果表明,通气局部空泡存在透明空泡区、气水混合区、脱落区以及尾涡区,其中存在复杂的环形涡形成、破碎以及脱落等过程,这些过程显著影响了通气局部空泡的发展过程. 在POD模态分析中,主要模态的分布区域与环形涡的形成、破碎区域高度相关,进而表明通气局部空泡的泡沫状旋涡脱落是由于环形涡的发展演化引起的.

     

    Abstract: As an easy way to implement drag reduction, ventilated cavitation has been widely used in the development of high-speed underwater vehicles. For underwater vehicles, ventilated partial cavity exhibits complex internal turbulent flow and shedding characteristics. A numerical simulation method based on boundary data immersion method (BDIM) and two-step projection method was established, ILES (implicit large eddy simulation) was used to numerically study the ventilation partial cavity, and POD (Proper Orthogonal Decomposition) modal analysis was employed to study the shedding turbulent structures of the ventilated partial cavity. The results show that ventilation partial cavities have transparent cavity region, gas-water mixing region, shedding region and tail vortex region, in which there are complex annular vortex formation, crushing and shedding processes, which significantly affect the development of ventilation partial cavities. In the POD modal analysis, the distribution region of the main modes is highly correlated with the formation and breaking region of the annular vortex, which indicates that the foam vortex shedding of ventilation partial cavities is caused by the development and evolution of the annular vortex.

     

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