徐顺, 刘琦, 张益诚, 等. 不同空化工况的导管桨梢隙涡空化流场数值分析[J]. 中国舰船研究, 2023, 18(3): 122–128. doi: 10.19693/j.issn.1673-3185.02760
引用本文: 徐顺, 刘琦, 张益诚, 等. 不同空化工况的导管桨梢隙涡空化流场数值分析[J]. 中国舰船研究, 2023, 18(3): 122–128. doi: 10.19693/j.issn.1673-3185.02760
XU S, LIU Q, ZHANG Y C, et al. Flow characteristics of tip leakage vortex cavitation ofducted propeller under different cavitation conditions[J]. Chinese Journal of Ship Research, 2023, 18(3): 122–128. doi: 10.19693/j.issn.1673-3185.02760
Citation: XU S, LIU Q, ZHANG Y C, et al. Flow characteristics of tip leakage vortex cavitation ofducted propeller under different cavitation conditions[J]. Chinese Journal of Ship Research, 2023, 18(3): 122–128. doi: 10.19693/j.issn.1673-3185.02760

不同空化工况的导管桨梢隙涡空化流场数值分析

Flow characteristics of tip leakage vortex cavitation ofducted propeller under different cavitation conditions

  • 摘要:
      目的  旨在研究梢隙涡(TLV)空化发展对涡核特性的影响规律。
      方法  结合SST k-ω 和Zwart-Gerber-Belamri空化模型,对不同空化工况下的导管桨梢隙涡空化流场开展数值模拟研究,然后在验证数值模拟可靠性的基础上,基于汽相体积分数等值面图和Q准则,分别对梢隙涡空化发展及涡核特性演变规律展开研究。
      结果  结果显示,梢隙涡空化的发展使得稳定的泄漏流空化面积不断扩大,当发展至特定工况时,梢隙涡空化会在泄漏空化的随边处发生旋拧;若空化继续发展,将对导管桨的性能产生显著影响。空化的发展使得梢隙涡逐渐远离叶片吸力面,并使涡心处的流速分布更为复杂,当空化数σ = 1.488时,空化的持续发展会显著降低梢隙涡的强度。随着梢隙涡向下游发展,梢隙涡卷吸来自壁面周向涡量的能力不断减弱,并且间隙处的湍动能会随着梢隙涡的发展逐渐输运至涡心处。
      结论  研究方法和研究结果可为水力旋转机械的性能预测和梢隙涡空化的控制提供相应的理论指导。

     

    Abstract:
      Objectives  This study aims to investigate the effects of the development of tip leakage vortex (TLV) cavitations on the core characteristics of vortices.
      Methods  The numerical simulation associated with the SST k-ω turbulence model and Zwart-Gerber-Belamri (ZGB) cavitation model is used to solve the cavitating flow of the TLV of a ducted propeller under different cavitation conditions. Based on the reliable numerical simulation, the development of the TLV cavitation and the evolution of its core characteristics are studied according to the vapor volume fraction iso-surface and Q criterion.
      Results  The results show that the area of the tip leakage cavitation expands with the development of the TLV cavitation. The TLV cavitation twists near the trailing edge of the tip leakage cavitation under specific conditions. The performance of the ducted propeller is greatly affected by the continuous decrease in the cavitation number. The development of the cavitation makes the TLV gradually flow away from the blade suction surface, increasing the complexity of the velocity distribution at the TLV core center. When the cavitation number σ is 1.488, the continuous development of the cavitation significantly reduces the intensity of the TLV. With the development of the TLV, its ability to absorb the circumferential vorticity from the inner wall weakens, and the turbulent kinetic energy from the tip gap is gradually transported to the vortex center.
      Conclusions  The proposed method and results of this study can provide valuable references for the performance prediction of hydraulic rotating machinery and control methods for TLV cavitations.

     

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