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A generic velocity-free calculation method of the blasting wave in nuclear power plants for designing venting system

机译:核电站设计通风系统爆破波的一种通用速度计算方法

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摘要

Venting system, mainly composed of bursting discs, is designed to protect the structural integrity of the cabins in nuclear power plants (NPPs). During a loss of coolant accident (LOCA), much gas is rapidly released into the cabin, forming a kind of pressure longitudinal wave (PLW) named "blasting wave" and challenge the mechanical strength of the envelope structure. Simulation of the blasting wave is meaningful for designing bursting discs. CFD is a generic method for cabins with arbitrary geometric features, which consumes much time and computing resource; There exists a mathematical model based on wave equation describing PLW, but it has never been applied in the field of nuclear reactor accident because of some bottlenecks. In this study, the mathematical model based on wave equation is transformed into a generic method of simulating PLW without solving velocity field, which is in the form of a velocity-free PDE problem with velocity-related initial and boundary conditions. The boundary condition is not Dirichlet, Neumann nor Robbin, and provides condition for one-dimensional analytical solution. The problem can also be solved by finite element method (FEM). Both solutions are validated by CFD simulation in our previous study and can be extended to higher dimensions. In engineering application, the analytical solution can be directly used if the cabin's geometry is relatively simple, while FEM solution can be used on a coarse meshing if the geometry is complex. Both applications are convenient compared with CFD method.
机译:通风系统主要由爆破盘组成,旨在保护核电站(NPPS)中舱室的结构完整性。在冷却液事故(基因座)的损失期间,大量气体迅速释放到舱室中,形成一种名为“爆破波”的压力纵波(PLW)并挑战包络结构的机械强度。爆破波的仿真对于设计爆破盘是有意义的。 CFD是具有任意几何特征的舱室的通用方法,其消耗了很多时间和计算资源;基于描述PLW的波动方程存在数学模型,但由于一些瓶颈,它从未应用于核反应堆事故领域。在该研究中,基于波动方程的数学模型被转换为模拟PLW的通用方法,无需求速度场,这是速度相关的初始和边界条件的无速度PDE问题。边界条件不是Dirichlet,Neumann和Robbin,并提供一维分析解决方案的条件。问题也可以通过有限元方法(FEM)来解决。在我们之前的研究中,CFD模拟验证了这两种解决方案,并且可以扩展到更高的维度。在工程应用中,如果机舱的几何形状相对简单,则可以直接使用分析解决方案,而如果几何形状复杂,则可以在粗地啮合上使用FEM解决方案。与CFD方法相比,这两个应用都很方便。

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