首页> 外文会议>AIAA aerospace sciences meeting including the new horizons forum and aerospace exposition >Unsteady Flow Simulation of a High-Lift configuration using a Lattice Boltzmann Approach
【24h】

Unsteady Flow Simulation of a High-Lift configuration using a Lattice Boltzmann Approach

机译:高格构型的非定常流动模拟,采用莱迪思·波尔兹曼方法

获取原文

摘要

A Lattice-Boltzmann Method (LBM) based approach combined with a very large eddy simulation (VLES) turbulence modeling is used for the unsteady simulation of the flow field around the high-lift configuration used in the first AIAA high-lift prediction workshop. The numerical approach as well as the meshing technique is briefly described. The simulations are conducted first for some selected angle of attacks and configurations prescribed within the workshop and compared to the available experimental results. Several investigations are presented including a resolution study, the influence of added geometrical details and the laminar to turbulence transition in the simulation. In a second step the simulation domain is extended to include the wind tunnel walls in an effort to predict the blockage and installation effects of the wind tunnel and compare with the uncorrected force and moment measurements.
机译:基于Lattice-Boltzmann方法(LBM)的方法与超大型涡流仿真(VLES)湍流模型相结合,用于在AIAA高升程预测研讨会中使用的高升程配置周围流场的不稳定模拟。简要介绍了数值方法和网格划分技术。首先针对车间内规定的某些选定的迎角和构型进行仿真,然后将其与可用的实验结果进行比较。提出了一些研究,包括分辨率研究,附加几何细节的影响以及模拟中层流到湍流的转变。第二步,将模拟域扩展到包括风洞壁,以预测风洞的阻塞和安装效果,并与未校正的力和力矩测量值进行比较。

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