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高能管道壁面摩擦对于蒸汽射流影响特性分析

徐焱明 信志强 何铮 蔡煜

徐焱明, 信志强, 何铮, 蔡煜. 高能管道壁面摩擦对于蒸汽射流影响特性分析[J]. 应用数学和力学, 2025, 46(2): 142-153. doi: 10.21656/1000-0887.450047
引用本文: 徐焱明, 信志强, 何铮, 蔡煜. 高能管道壁面摩擦对于蒸汽射流影响特性分析[J]. 应用数学和力学, 2025, 46(2): 142-153. doi: 10.21656/1000-0887.450047
XU Yanming, XIN Zhiqiang, HE Zheng, CAI Yu. Characteristic Analysis on Effects of High-Energy Pipe Wall Friction on Steam Jets[J]. Applied Mathematics and Mechanics, 2025, 46(2): 142-153. doi: 10.21656/1000-0887.450047
Citation: XU Yanming, XIN Zhiqiang, HE Zheng, CAI Yu. Characteristic Analysis on Effects of High-Energy Pipe Wall Friction on Steam Jets[J]. Applied Mathematics and Mechanics, 2025, 46(2): 142-153. doi: 10.21656/1000-0887.450047

高能管道壁面摩擦对于蒸汽射流影响特性分析

doi: 10.21656/1000-0887.450047
基金项目: 

国家自然科学基金 11872174

详细信息
    作者简介:

    徐焱明(1999—),男,硕士生(E-mail: 221308010035@hhu.edu.cn)

    通讯作者:

    信志强(1983—),男,副教授,博士(通讯作者. E-mail: xinzhiqiang@hhu.edu.cn)

  • 中图分类号: O358;TK212+.3

Characteristic Analysis on Effects of High-Energy Pipe Wall Friction on Steam Jets

  • 摘要: 以双端断裂后的高能管道为研究对象,对蒸汽射流过程进行了数值模拟. 研究了滞止压力、管道壁面摩擦对喷射锥和射流冲击力的影响,总结了喷射锥内速度、温度、压力的规律. 并将不同入口条件下的射流冲击力与使用设计准则计算结果进行了比较,探究了设计准则在超出适用压力范围时,有关公式和方法的适用性. 模拟结果表明,蒸汽射流在出破口平面后一段距离内,压力和温度迅速下降,速度迅速上升,随后均有波动变化,最终随着逐渐远离喷嘴出口,速度、温度逐渐下降,压力趋近于大气压. 喷射锥初始扩散角度、射流影响范围及射流冲击力与入口压力正相关,与喷管壁面粗糙度负相关. 设计准则对射流初始扩散角度的假设不具有普遍性,当压力较大时,实际射流初始扩散角度大于规范规定的45°. 设计准则评定冲击射流全部喷射到平板的冲击效应时,标准对于理想无摩擦的管道喷射冲击力可以精准预测,但使用标准对实际有壁面摩擦的管道射流冲击力进行评估时,会存在一定偏差,且随着壁面粗糙度和压力的增加,评估偏差程度会增大.
  • 图  1  计算区域示意图

    Figure  1.  The sketch of the computational domain

    图  2  网格剖面图

    Figure  2.  The cross section of the mesh

    图  3  网格无关性验证结果

       为了解释图中的颜色,读者可以参考本文的电子网页版本,后同.

    Figure  3.  Grid independence verification results

    图  4  模型验证结果

       为了解释图中的颜色,读者可以参考本文的电子网页版本,后同.

    Figure  4.  Model validation results

    图  5  不考虑摩擦时速度分布云图

    Figure  5.  Velocity distributions of frictionless cases

    图  6  不考虑摩擦时温度分布云图

    Figure  6.  Temperature distributions of frictionless cases

    图  7  中心轴线上速度分布

    Figure  7.  Velocity distributions on the central axis

    图  8  中心轴线上温度分布

    Figure  8.  Temperature distributions on the central axis

    图  9  不考虑摩擦时压力分布云图

    Figure  9.  Pressure distributions of frictionless cases

    图  10  中心轴线上压力分布

    Figure  10.  Pressure distributions on the central axis

    图  11  中心轴线上的无量纲压力、速度、温度分布(入口压力6.90 MPa,喷管壁面粗糙度0.000 0 mm)

    Figure  11.  Dimensionless pressure velocity and temperature changes on the central axis (inlet pressure 6.90 MPa, pipe wall roughness 0.000 0 mm)

    图  12  6.90 MPa时冲击射流速度云图

    Figure  12.  The jet impact velocity distribution at 6.90 MPa

    图  13  圆盘径向总压力分布

    Figure  13.  Radial total pressure distributions on the disk

    图  14  不同条件下圆盘所受喷射冲击力

    Figure  14.  Jet impingement forces on the disk under different conditions

    表  1  不同条件下圆盘所受喷射冲击力(单位: N)

    Table  1.   Jet impingement forces on the disk under different conditions (unit: N)

    6.90 MPa 13.80 MPa 20.00 MPa
    predicted value 430.67 867.68 1 260.36
    Δ=0.000 0 mm 419.67 859.16 1 251.19
    Δ=0.012 5 mm 368.63 751.59 1 091.79
    Δ=0.025 0 mm 358.03 726.69 1 055.70
    Δ=0.125 0 mm 323.54 652.03 948.35
    下载: 导出CSV
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出版历程
  • 收稿日期:  2024-03-26
  • 修回日期:  2024-04-24
  • 刊出日期:  2025-02-01

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