...
首页> 外文期刊>AIAA Journal >Statistical Vortex-Generator-Jet Model for Turbulent Flow Separation Control
【24h】

Statistical Vortex-Generator-Jet Model for Turbulent Flow Separation Control

机译:涡流分离控制的统计涡-发生器-射流模型

获取原文
获取原文并翻译 | 示例
           

摘要

This contribution describes the development and evaluation of a new statistical modeling approach for active vortex generator jets. Previous experiments from the Technische Universitat Braunschweig and their subsequent evaluation by the present authors showed that the induced flowfield can be reasonably well represented by two-dimensional Lamb-Oseen vortices. Based on that, an analytical expression for the Lamb-Oseen-vortex-model maximum circulation Γ_(max) was derived in terms of the freestream velocity U_∞ the jet-to-freestream velocity ratio λ, and the jet skew angle β, as well as the actuator diameter Φ_(vgj)- Based on the parameterized results, universal values for the Lamb-Oseen-vortex-model parameters at the actuator position were determined for the development of the statistical vortex-generator-jet model. The idea behind the statistical modeling approach is that the vortices are represented by their spanwise-averaged velocity correlations, or vortex stresses, that are added to the turbulence stresses in a Reynolds stress turbulence model. The spanwise-averaged vortex stresses are derived by computing the spanwise-averaged second-order statistics of the vortex flowfield. These vortex-generator-jet model results were compared to the spanwise-averaged vortex stresses from experiments and from fully resolved computational fluid dynamics investigations, and reasonable qualitative as well as quantitative agreement was found.
机译:这项贡献描述了用于主动涡流发生器射流的新统计建模方法的开发和评估。不伦瑞克工业大学的先前实验及其作者的后续评估表明,诱导流场可以用二维Lamb-Oseen涡旋很好地表示。在此基础上,根据自由流速度U_∞,射流与自由流速度比λ以及射流偏斜角β,得出了Lamb-Oseen-涡模型最大循环Γ_(max)的解析表达式。以及致动器直径Φ_(vgj)-基于参数化结果,确定致动器位置处的Lamb-Oseen-涡模型参数的通用值,以开发统计涡发生器-喷气模型。统计建模方法背后的思想是,涡旋由其跨度平均速度相关性(即涡旋应力)表示,它们在雷诺应力湍流模型中被添加到湍流应力中。通过计算涡流场的翼展方向平均二阶统计量,可以得出翼展方向平均涡旋应力。将这些涡流发生器喷射模型的结果与实验和完全解析的计算流体动力学研究的翼展方向平均涡流应力进行比较,发现了合理的定性和定量协议。

著录项

  • 来源
    《AIAA Journal》 |2013年第5期|1119-1129|共11页
  • 作者单位

    Royal Institute of Technology, 100 44 Stockholm, Sweden;

    Information and Aeronautical Systems, FOI Swedish Defence Research Agency and Linne Flow Centre;

    Royal Institute of Technology, 100 44 Stockholm, Sweden;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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