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基于传递矩阵法的螺旋十字形燃料棒流致振动响应分析

FLOW-INDUCED VIBRATION RESPONSE ANALYSIS OF A HELICAL CRUCIFORM FUEL ROD BASED ON TRANSFER MATRIX METHOD

  • 摘要: 螺旋十字形燃料棒(Helical Cruciform Fuel, HCF)是一种新型燃料棒, 具有良好的热工水力性能和自支撑约束特征. 针对现有基于 Workbench 平台的流固耦合分析在燃料棒流致振动响应计算中存在计算成本较高、收敛调试复杂等问题, 本文基于欧拉-伯努利梁理论, 构建了一套结合传递矩阵法(Transfer Matrix Method, TMM)与模态叠加法(Modal Superposition Method, MSM)的高效分析框架. 首先, 采用平行移轴定理计算 HCF 棒不同轴向位置处的截面惯性矩; 随后, 基于 TMM 推导 HCF 棒的传递矩阵, 求解其固有频率与振型, 并采用有限元法(Finite Element Method, FEM)验证模态计算结果; 进一步, 通过大涡模拟获得棒表面的湍流激振力, 利用 MSM 计算流致振动响应. 结果表明: TMM 与 FEM 得到的前三阶固有频率基本一致, 跨中位置均方根位移的相对误差约为 0.01%, 两种方法预测的振型、时频响应及振动轨迹均高度吻合. 在文中所列算例与计算配置下, 所提出方法的总计算时间约为参考 Workbench 方法的四分之一, 且结构响应求解时间仅约为 4.5 min. 本文所构建的分析框架能够在保证计算精度的同时提高 HCF 棒流致振动响应的计算效率, 可为大规模燃料棒束的流固耦合分析提供一定的参考价值.

     

    Abstract: The helical cruciform fuel (HCF) rod is a novel fuel rod, which exhibits favorable thermal-hydraulic performance and a self-supporting structural configuration. However, conventional Workbench-based fluid-structure interaction analyses of flow-induced vibration (FIV) are computationally expensive and often require substantial effort to achieve numerical convergence. To address these limitations, an efficient analytical framework integrating the transfer matrix method (TMM) and modal superposition method (MSM) was developed based on Euler-Bernoulli beam theory. First, the cross-sectional moment of inertia at different axial positions of the HCF rod was determined using the parallel-axis theorem. The transfer matrix of the HCF rod was then derived to calculate its natural frequencies and mode shapes, and the modal results were verified against those obtained using the finite element method (FEM). Subsequently, the turbulent excitation forces acting on the fuel rod were obtained through large-eddy simulation, and the FIV response was calculated using the MSM. The results show that the first three natural frequencies predicted by the TMM agree closely with the results by FEM. The relative difference in the root-mean-square displacement at the midspan is approximately 0.01%, and the predicted mode shapes, time- domain and frequency-domain responses, and vibration trajectories are in close agreement. For the cases and computational configurations considered, the total computation time of the proposed framework is approximately one quarter of that of the referenced Workbench-based method, while the structural response calculation requires only about 4.5 min. The proposed framework improves computational efficiency while maintaining high accuracy and provides a practical approach for the FIV analysis of large-scale fuel rod bundles.

     

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