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Boundary layer analysis of ventilated partial cavity for friction drag reduction

机译:摩擦减阻通风局部腔边界层分析

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摘要

This paper describes the use of water tunnel plate experiments and large eddy simulations to understand ventilated partial cavity (VPC) flow, especially the mechanism of friction drag reduction. The different flow behaviors along the flow direction indicate that VPC can be divided into three regions: continuous cavity, transitional cavity, and mixing cavity. Specifically, in the continuous cavity region, the flow state can be regarded as laminar; the density and dynamic viscosity are close to those of the strictly gas phase; and the resulting wall shear stress reaches minimum level along the flow direction. In the transitional cavity region, the flow state is similar to the transition state of single-phase flow with density, viscosity, and wall shear stress along the flow direction all exhibiting exponential growth. In the mixing cavity region, the flow state is analogous to turbulence. The flow is in a phase mixed state. The dynamic viscosity is close to that of the strictly water phase. The resulting wall shear stress is stable with small fluctuations. Importantly, the analytical boundary layer equation for wall shear stress derived from the momentum equation remains applicable to the continuous cavity and the mixing cavity regions.
机译:本文介绍了水隧道板实验和大型涡流模拟,以了解通风的部分腔(VPC)流动,尤其是摩擦减阻的机制。沿着流动方向的不同流动表明VPC可以分为三个区域:连续腔,过渡腔和混合腔。具体地,在连续腔区域中,流动状态可以被视为层状;密度和动态粘度接近严格气相的粘度;并且所得到的壁剪切应力沿着流动方向达到最小水平。在过渡腔区域中,流动状态类似于单相流的过渡状态,其具有密度,粘度和沿着流动方向的壁剪切应力,所有表现出指数增长。在混合腔区域中,流动状态类似于湍流。流动处于相位混合状态。动态粘度接近严格水相的粘度。由此产生的壁剪切应力具有小波动稳定。重要的是,源自动量方程的壁剪切应力的分析边界层方程仍然适用于连续腔和混合腔区域。

著录项

  • 来源
    《Ocean Engineering》 |2021年第1期|109799.1-109799.22|共22页
  • 作者单位

    Zhejiang Univ Coll Energy Engn Hangzhou 310027 Peoples R China;

    Zhejiang Univ Coll Energy Engn Hangzhou 310027 Peoples R China;

    Zhejiang Univ Coll Energy Engn Hangzhou 310027 Peoples R China;

    Zhejiang Univ Coll Energy Engn Hangzhou 310027 Peoples R China|Zhejiang Univ State Key Lab Fluid Power & Mech Syst Hangzhou 310027 Peoples R China;

    Zhejiang Univ Ocean Coll Zhoushan 316021 Peoples R China;

    Zhejiang Univ Coll Energy Engn Hangzhou 310027 Peoples R China|Shanghai Ship & Shipping Res Inst Shanghai 200135 Peoples R China;

  • 收录信息
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Drag reduction; Boundary layers; Gas-liquid multiphase flow; Ventilated partial cavity; Large eddy simulation;

    机译:减少;边界层;气液多相流动;通风局部腔;大涡模拟;

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