首页> 外文会议>AIAA fluid dynamics conference;AIAA aviation forum >Using Adaptive Mesh Refinement to Study Grid Resolution Effects for Shock/Boundary-Layer Interactions
【24h】

Using Adaptive Mesh Refinement to Study Grid Resolution Effects for Shock/Boundary-Layer Interactions

机译:使用自适应网格细化研究冲击/边界层相互作用的网格分辨率效果

获取原文

摘要

Adaptive Mesh Refinement (AMR) promises a much more computationally efficient means to obtain a discrete approximation to a continuous boundary value problem of a specified accuracy than classic isotropic grid refinement. The AMR capability of OVERFLOW is utilized to provide estimates of the exact analytical solutions to problems of interest for turbulence modeling. Predictions of surface pressure and skin friction, essentially the state of stress at the surface, shows little difference with grids believed to be "grid resolved." Velocity profiles, on the other hand, show marked differences in flows with shocks. The AMR method, as implemented in OVERFLOW 2.2k, appears to provide the ability to produce arbitrarily accurate solutions at a predictable cost much smaller than classic uniform mesh refinement.
机译:自适应网格细化(AMR)与经典的各向同性网格细化相比,它提供了一种计算效率更高的方法,以获得具有指定精度的连续边界值问题的离散逼近。 OVERFLOW的AMR功能可用于对湍流建模感兴趣的问题提供精确解析解决方案的估计。表面压力和皮肤摩擦的预测,本质上是表面的应力状态,与被认为是“网格分解”的网格几乎没有差异。另一方面,速度曲线显示了在冲击作用下流量的明显差异。在OVERFLOW 2.2k中实现的AMR方法似乎提供了以比传统的均匀网格细化要小的得多的可预测成本生成任意精确解的能力。

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