The wave evolution and pressure distribution characteristics of the interaction between long-duration blast load and cylindrical structure
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摘要: 长脉宽爆炸波与结构作用的波传播及其载荷分布规律是大型爆炸防护设计与安全评估的重要基础。为了掌握长脉宽爆炸波与圆柱壳的相互作用机制及其作用下圆柱壳表面的载荷分布规律，开展了100 ms级冲击波圆柱绕流的激波管试验，并采用大涡模拟方法和高阶WENO-TCD（weighted essentially non-oscillatory-tuned centered difference）混合格式进一步对150 ms长脉宽冲击波与圆柱作用过程的波系演化与压力分布进行了数值分析。结果表明：数值仿真与压力实测结果吻合较好，长脉宽作用下圆柱壳载荷分布呈现出明显的角度和高度相关性，背面压力高于侧面甚至与迎爆面相当，具有不同于传统短脉宽冲击波传播中的压力衰减模式。流场的压力云纹和波系三维结构演化揭示了侧端面的突然扩张是压力初期震荡及相比于正面和背面压力更低的主要原因；系列绕射激波在壳体背面碰撞与反射，以及序列减速激波在135°相位附近的驻定与叠加作用，是引起背面压力呈现出载荷整体提升的主要机制。此外，背风面上尾涡结构的形成与演化过程受边界效应的影响是导致长脉宽圆柱壳载荷分布沿高度方向出现差异的关键因素。Abstract: The wave propagation and pressure distribution during the interaction between long duration blast waves and structures are important foundations for the large scale explosion protection design and safety assessment. In order to understand the interaction mechanism between long duration blast waves and cylindrical shells, as well as the distribution law of the surface load on the cylindrical shells under their action, the overpressure histories on the cylindrical structure surface were obtained through the 150ms long duration blast wave shock tube experiment, and the shock wave evolution and the pressure load distribution were investigated numerically using the large eddy simulation and hybrid WENO-TCD (weighted essentially non-oscillatory-tuned centered difference) method. The results show that the overpressure load of the calculation results is in good agreement with the experimental results, and the overpressure load on the cylindrical shell appears a clear angle and height correlation. The pressure on the back shell is higher than that on the side surface or even comparable to the blast on the facing surface, which exhibit different pressure attenuation modes from the traditional short duration blast wave propagation. The sudden expansion on the side surface is the main reason for the initial oscillation of pressure, and has a lower pressure than that at the windward and leeward sides. On the other hand, a series of diffracted shock waves collides and reflects on the symmetry plane of the shell leeward, as well as the stationary and superimposed effects of the series of decelerating shock waves near the 135° phase, which are the main mechanisms that cause the overall increase of the pressure load on the cylindrical shell. In addition, the formation and evolution of wake vortex structures on the leeward side due to the boundary effects is a key factor leading to differences in the load distribution along the height direction. The above analysis methods and related results lay the foundation for the subsequent study of load distribution models for typical structural components under long duration blast waves.
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Key words:
- long-duration /
- blast waves /
- cylindrical shell structures /
- shock waves experiment
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图 5 不同网格尺度下圆柱壳体表面压力载荷分布曲线
Figure 5. Grid scales effect on the surface pressure load distribution curves of cylindrical shell
图 6 H = 0.9 m时，表面压力监测点计算结果与测试结果的对比
Figure 6. Comparison of the overpressure with the corresponding experimental results at H = 0.9 m
图 7 H = 0 m时，圆柱壳体表面压力载荷变化曲线
Figure 7. The overpressure histories on the surface of cylindrical structure at H = 0 m
图 8 H = 0 m时，压力载荷峰值沿角度的分布曲线
Figure 8. Distribution of the peak overpressure along phase at H = 0 m
图 9 长脉宽平面冲击波与圆柱壳体作用过程的密度纹影图（H = 0 m）
Figure 9. Numerical schlieren image of the interaction between long-duration blast and cylindrical structure at H = 0 m
图 11 H = 0 m时，入射激波I1-4与壳体作用过程中壳体表面4个测点压力载荷变化曲线
Figure 11. The overpressure on the surface of cylindrical structure at H = 0 m
图 12 长脉宽平面冲击波与圆柱壳体作用过程中壳体表面压力分布图（左图为云纹图；中间为迎爆面压力分布；右图为背部压力分布）
Figure 12. Pressure distribution on the surface of a cylindrical structure (The left image is a moir é pattern; the middle is the pressure distribution on the blasting surface; the right image is the pressure distribution on the back)
图 13 不同方位处，圆柱壳体表面压力载荷变化曲线
Figure 13. Overpressure load on the surface of cylindrical structure at different orientations
图 14 测点压力载荷峰值沿角度和高度的分布规律
Figure 14. Distribution of the peak overpressure along the angle and height
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