首页> 外文OA文献 >Numerical simulations of two-dimensional and three-dimensional shock wave/turbulent boundary layer interactions
【2h】

Numerical simulations of two-dimensional and three-dimensional shock wave/turbulent boundary layer interactions

机译:二维和三维冲击波/湍流边界层相互作用的数值模拟

摘要

The impinging shock-wave/flat-plate boundary layer interaction is a standard CFD case for two-dimensional (2D) SWTBLI, which represents the simplest SWTBLI configuration for the validation of turbulence models and computational methods. Although plenty of researches focused on this kind of flows2-5, the flow mechanism in it is still not well understood. Comparing with the 2D SWTBLI, the three-dimensional (3D) SWTBLI is even less studied and understood, although, it is closer to real flows and has special influences on the performances of intakes and control surfaces. Most researches of 3D SWTBLI are limited in the framework of experimental measurements6-12 and numerical simulations by solving Reynolds-averaged Navier–Stokes (RANS) equations13-16. The large-eddy simulation (LES) or direct numerical simulation (DNS), which can give detailed information of turbulent flows and greatly benefits the research of turbulence mechanisms, has not been applied in the 3D SWTBLI yet in published reports
机译:冲击波/平板边界层的碰撞是二维(2D)SWTBLI的标准CFD情况,它代表用于验证湍流模型和计算方法的最简单的SWTBLI配置。尽管大量研究集中在这种流[2-5],但其中的流机制仍未得到很好的理解。与2D SWTBLI相比,对三维(3D)SWTBLI的研究和了解更少,尽管它更接近实际流量,并且对进气和操纵面的性能有特殊影响。 3D SWTBLI的大多数研究都局限于实验测量6-12和通过求解雷诺平均Navier-Stokes(RANS)方程13-16进行的数值模拟的框架中。大涡模拟(LES)或直接数值模拟(DNS)可以提供详细的湍流信息,极大地有利于湍流机理的研究,尚未在3D SWTBLI中应用。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利

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