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孤立波浪边界干扰下流线型箱梁气动特性

殷瑞涛 祝兵 田源 杨镇宇 杨志莹

殷瑞涛, 祝兵, 田源, 杨镇宇, 杨志莹. 孤立波浪边界干扰下流线型箱梁气动特性[J]. 西南交通大学学报, 2023, 58(2): 398-405, 413. doi: 10.3969/j.issn.0258-2724.20210211
引用本文: 殷瑞涛, 祝兵, 田源, 杨镇宇, 杨志莹. 孤立波浪边界干扰下流线型箱梁气动特性[J]. 西南交通大学学报, 2023, 58(2): 398-405, 413. doi: 10.3969/j.issn.0258-2724.20210211
YIN Ruitao, ZHU Bing, TIAN Yuan, YANG Zhenyu, YANG Zhiying. Aerodynamic Performance of Streamlined Box Girder Under Interferences from Solitary Wave Boundary[J]. Journal of Southwest Jiaotong University, 2023, 58(2): 398-405, 413. doi: 10.3969/j.issn.0258-2724.20210211
Citation: YIN Ruitao, ZHU Bing, TIAN Yuan, YANG Zhenyu, YANG Zhiying. Aerodynamic Performance of Streamlined Box Girder Under Interferences from Solitary Wave Boundary[J]. Journal of Southwest Jiaotong University, 2023, 58(2): 398-405, 413. doi: 10.3969/j.issn.0258-2724.20210211

孤立波浪边界干扰下流线型箱梁气动特性

doi: 10.3969/j.issn.0258-2724.20210211
基金项目: 国家自然科学基金(U1834207)
详细信息
    作者简介:

    殷瑞涛(1995—),男,博士研究生,研究方向为跨海桥梁风浪耦合动力学,E-mail: yinruitao@my.swjtu.edu.cn

    通讯作者:

    祝兵(1965—),男,教授,研究方向为桥梁结构动力学及桥梁风浪耦合动力学,E-mail:zhubing126@126.com

  • 中图分类号: U441.3

Aerodynamic Performance of Streamlined Box Girder Under Interferences from Solitary Wave Boundary

  • 摘要:

    近海流线型箱梁主梁距水面较低时,气动特性极易受到极端波浪边界的干扰.为研究极端波浪边界干扰下流线型箱梁气动特性,以孤立波浪模拟极端波浪,基于FLUENT软件,采用铺层网格技术建立了模拟运动孤立波浪边界干扰下流线型箱梁气动特性的数值模型;利用所建立并验证的数值模型研究了不同参数下运动孤立波浪边界对流线型箱梁气动特性(静气动力系数、涡量场以及平均压力系数和脉动压力系数分布)的干扰. 分析结果表明:不同孤立波浪边界运动速度干扰下流线型箱梁气动特性明显区别于无波浪工况;随波浪边界运动,迎风角处剪切层方向相比于梁底转折角处(8° 风攻角)及梁顶转折角处(−8° 风攻角)剪切层方向变化明显;在运动孤立波浪边界干扰下,箱梁抖振响应会随风攻角幅值增大呈增大趋势.

     

  • 图 1  流线型箱梁原型图(单位:cm)

    Figure 1.  Prototype of the streamlined box girder (unit:cm)

    图 2  计算区域划分

    Figure 2.  Configuration of the computational fluid domain

    图 3  部分计算网格划分图

    Figure 3.  Partial computational grid details

    图 4  三分力正方向及压力测点位置

    Figure 4.  Positive directions of the aerostatic force coefficients and positions of the pressure measuring points

    图 5  风洞试验模型

    Figure 5.  Model of the test model in the wind tunnel

    图 6  不同v/U及无波浪工况下三分力系数变化曲线

    Figure 6.  Variation curves of aerostatic force coefficients under different v/U and no-wave cases

    图 7  不同风攻角α下三分力系数变化曲线

    Figure 7.  Variation curves of aerostatic force coefficients under different wind attack angles α

    图 8  α=0° 时${\overline C}_{\mathrm{p}}$${\widetilde C}_{\mathrm{p}}$分布(负值指向截面外侧)

    Figure 8.  ${\overline C}_{\mathrm{p}}$ and ${\widetilde C}_{\mathrm{p}}$ distributions for α=0° (negative values point outward the section)

    图 9  α=8° 涡量图

    Figure 9.  Vorticity magnitude field for α=8°

    图 10  α=8° 时${\overline C}_{\mathrm{p}}$${\widetilde C}_{\mathrm{p}}$分布

    Figure 10.  ${\overline C}_{\mathrm{p}}$ and ${\widetilde C}_{\mathrm{p}}$ distributions for α=8°

    图 11  α=−8° 涡量图

    Figure 11.  Vorticity magnitude field for α=−8°

    图 12  α=−8° 时${\overline C}_{\mathrm{p}}$${\widetilde C}_{\mathrm{p}}$分布

    Figure 12.  ${\overline C}_{\mathrm{p}}$ and ${\widetilde C}_{\mathrm{p}}$ distributions for α=−8°

    表  1  典型工况风洞试验与数值模拟结果对比

    Table  1.   Comparison of results between the wind tunnel test and numerical simulation of typical cases

    h1/mx/Bα/ (°)${ {\overline{C}}_{ {\rm{d} } } }$${ {\overline{C}}_{ {\rm{l} } } }$${ {\overline{C}}_{ {\rm{m} } } }$
    试验CFD试验CFD试验CFD
    0.48−1.0−4 0.0430.035−0.803−0.747−0.198−0.189
    0.48−0.5−4 0.1160.105−0.870−0.809−0.196−0.185
    0.480 −4 0.6140.555−0.560−0.625−0.080−0.076
    0.48 0.5−4 0.8100.797−0.543−0.641−0.008−0.014
    0.48 1.0−4 0.6570.632−0.413−0.502−0.010−0.016
    0.48−1.000.0690.071−0.550−0.540−0.097−0.088
    0.48−0.500.1100.102−0.514−0.496−0.079−0.062
    0.480 00.2800.255−0.359−0.426 0.035 0.029
    0.48 0.500.5010.462−0.196−0.222 0.137 0.100
    0.48 1.000.3260.358−0.021−0.026 0.127 0.092
    0.48−1.040.0340.029−0.206−0.262 0.017 0.026
    0.48−0.540.0810.076−0.255−0.313 0.045 0.044
    0.480 40.1070.098−0.089−0.106 0.175 0.141
    0.48 0.540.3170.286 0.331 0.267 0.218 0.203
    0.48 1.040.3010.279 0.504 0.422 0.199 0.190
    下载: 导出CSV
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出版历程
  • 收稿日期:  2021-03-22
  • 修回日期:  2021-06-25
  • 网络出版日期:  2022-11-14
  • 刊出日期:  2021-09-09

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