...
首页> 外文期刊>International Journal for Numerical Methods in Fluids >Computational study of curved shock-vortex interaction
【24h】

Computational study of curved shock-vortex interaction

机译:弯曲激涡相互作用的计算研究

获取原文
获取原文并翻译 | 示例
   

获取外文期刊封面封底 >>

       

摘要

The interaction between a curved shock wave and a compressible vortex is numerically investigated. The investigation concentrates on the local deformation of the shock structure due to the shock-vortex interaction. The essentially non-oscillatory(ENO) scheme is used to solve the unsteady two-dimensional Euler equations. A curved shock wave is obtained by the diffraction of an initially planar shock wave around a right-angled corner and then allowed to interact with a strong compressible vortexsuperimposed on the flow. The same vortex affects the shock wave differently depending on the placement of the vortex because of the varying strength of the shock wave. This effect could range from a non-symmetric deformation of the shock wave to a localdisruption in the shock structure depending on the strength of the shock wave in the interaction region. This process leading to a local disruption in the shock structure is analyzed in detail. It is shown that such a disruption in the shock structure can be predicted by simple one-dimensional considerations.
机译:数值研究了弯曲冲击波和可压缩涡旋之间的相互作用。研究集中在由于激涡相互作用引起的激波结构的局部变形上。使用本质上非振荡的(ENO)方案来求解不稳定的二维Euler方程。弯曲的冲击波是通过绕直角拐角处的初始平面冲击波进行衍射获得的,然后使其与叠加在流上的强可压缩涡旋相互作用。由于涡波强度的变化,相同的涡流会根据涡流的位置对冲击波产生不同的影响。取决于相互作用区域中冲击波的强度,这种影响的范围可能从冲击波的非对称变形到冲击结构中的局部破坏。详细分析了导致冲击结构局部破坏的过程。已经表明,可以通过简单的一维考虑来预测冲击结构的这种破坏。

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