首页> 外文会议>AIAA aviation forum >Turbulent / Non-Turbulent Interface and Uniform Momentum Zones of High-Speed Turbulent Boundary Layers Subjected to Streamline Pressure Gradients
【24h】

Turbulent / Non-Turbulent Interface and Uniform Momentum Zones of High-Speed Turbulent Boundary Layers Subjected to Streamline Pressure Gradients

机译:受流线压力梯度影响的高速湍流边界层的湍流/非湍流界面和均匀动量区

获取原文

摘要

The turbulenton-turbulent interface (TNTI) and uniform momentum zones (UMZ) within fully developed high-speed turbulent boundary layers subjected to streamline pressure gradients are investigated. Both favorable and adverse pressure gradients are generated using wall curvature in a Mach 4.9 freestream flow. The pressure gradient effects on the boundary layer mean properties and turbulent statics have been previously reported by [1] and [2] for FPU and APG, respectively. In the present work, the average TNTI height was shown to decrease with strong favorable pressure gradient, indicating reduced turbulence strength. The TNTI length per unit streamwise length increased for the SFPG case and slightly decreased for the APG cases. Together, the observed changes in TNTI height and length indicate that the curvature-driven pressure gradients are non-linearly affecting the TNTI by bringing it deeper into the boundary layer while simultaneously increasing the surface area of the interface for the SFPG case. Uniform momentum zones were also observed in the high-speed turbulent boundary layers. Qualitatively, the number of UMZs was seen to increase with more favorable pressure gradient even while the TNTI moved lower in the boundary layer. An outstanding question is the influence of compressibility on the structure of the TNTI and UMZs within a turbulent boundary layer. The majority of studies of TNTI and UMZs have focused on low Reynolds number, incompressible flows and as such, the quantitative conclusions drawn from those works may not apply to the present data. Further investigation into these compressibility effects are warranted and underway.
机译:研究了经受流线压力梯度的充分发展的高速湍流边界层内的湍流/非湍流界面(TNTI)和均匀动量区(UMZ)。在Mach 4.9自由流中,利用壁曲率会产生有利和不利的压力梯度。压力梯度对边界层平均特性和湍流静力的影响先前已由[1]和[2]分别报道过FPU和APG。在目前的工作中,显示出平均TNTI高度随着强烈的有利压力梯度而降低,表明湍流强度降低。对于SFPG,每单位流向长度的TNTI长度增加,对于APG,每单位TNTI长度略有减少。总之,观察到的TNTI高度和长度的变化表明,曲率驱动的压力梯度通过使TNTI更深地进入边界层,同时增加SFPG外壳的界面表面积,非线性地影响TNTI。在高速湍流边界层中也观察到均匀的动量区。定性地,即使TNTI在边界层中移动得更低,UMZ的数量也随着压力梯度的增加而增加。一个悬而未决的问题是可压缩性对湍流边界层中TNTI和UMZ的结构的影响。 TNTI和UMZ的大多数研究都集中在低雷诺数,不可压缩流动方面,因此,从这些工作得出的定量结论可能不适用于当前数据。有必要对这些可压缩性影响进行进一步研究。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号