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Fully Local Amplification Factor Transport Equation for Stationary Crossflow Instabilities

机译:平稳横流不稳定性的全局部放大因子传输方程

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摘要

The traditional linear stability analysis for transition prediction includes the following steps: solving velocity profiles using boundary-layer equations or a computational fluid dynamics solver, guessing and searching operations for the eigenvalues, computing the linear perturbation equations, and integrating the amplification factor N. It is difficult to implement into modern computational fluid dynamics solvers with parallel computations because it requires many nonlocal variables and coordinate system transformations. In this Paper, an amplification factor transport equation, which can be coupled with a modern computational fluid dynamics parallel solver, is established based on the analysis results through linear stability theory for stationary crossflow instabilities. According to the analysis results of Falkner-Skan-Cooke similarity velocity profiles using linear stability theory analysis, the source term of the present transport equation is formulated locally to describe the growth of stationary cross& W waves in the laminar boundary layer. This new equation is added to the NTs equation proposed by Coder and Maughmer for Tollmien-Schlichting instabilities. Finally, coupling of these two amplification factor transport equations and Menter's shear stress transport turbulence model completes an effective transition turbulence model. Comparisons between the present predictions, wind tunnel experiments and the standard linear stability theory analysis on an NLF(2)-0415 infinite swept wing, Petzold's sickle-shaped wing and 6:1 inclined prolate spheroid validate the reasonable establishment of the present amplification factor transport equation for stationary crossflow instabilities.
机译:传统的用于过渡预测的线性稳定性分析包括以下步骤:使用边界层方程或计算流体力学求解器求解速度剖面,对特征值进行猜测和搜索运算,计算线性摄动方程以及积分放大因子N。由于它需要许多非局部变量和坐标系转换,因此很难用并行计算实现到现代计算流体动力学求解器中。本文基于线性稳定理论的稳定横流不稳定性分析结果,建立了可与现代计算流体力学并行求解器耦合的放大因子传递方程。根据使用线性稳定性理论分析的Falkner-Skan-Cooke相似速度分布图的分析结果,本输运方程的源项在局部公式化,以描述层状边界层中平稳的横波和W波的增长。这个新方程式被添加到Coder和Maughmer为Tollmien-Schlichting不稳定性提出的NTs方程式中。最后,将这两个放大因子传递方程与Menter的切应力传递湍流模型耦合起来,就可以完成有效的过渡湍流模型。在NLF(2)-0415无限扫掠机翼,Petzold镰形镰状机翼和6:1倾斜长球体上进行的当前预测,风洞实验和标准线性稳定性理论分析之间的比较验证了当前放大因子传输的合理建立平稳横流不稳定性方程。

著录项

  • 来源
    《AIAA Journal》 |2019年第7期|2682-2693|共12页
  • 作者单位

    Imperial Coll London 180 Queens Gate London SW7 2AZ England|Tianjin Univ Sch Math Tianjin 300072 Peoples R China|Tianjin Univ Ctr Appl Math Tianjin 300072 Peoples R China;

    Northwestern Polytech Univ Sch Aeronautics Xian 710072 Shaanxi Peoples R China;

    Xi An Jiao Tong Univ State Key Lab Strength & Vibrat Mech Struct Sch Astronaut & Aeronaut Xian 710049 Shaanxi Peoples R China;

  • 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

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