首页> 外文期刊>Journal of propulsion and power >Dynamic Hybrid Reynolds-Averaged Navier-Stokes/Large-Eddy Simulation of a Supersonic Cavity
【24h】

Dynamic Hybrid Reynolds-Averaged Navier-Stokes/Large-Eddy Simulation of a Supersonic Cavity

机译:超音速腔的动态混合雷诺平均纳维-斯托克斯/大涡模拟

获取原文
获取原文并翻译 | 示例
           

摘要

A Mach 2 experimental supersonic cavity is simulated using a novel dynamic hybrid Reynolds-averaged Navier-Stokes/large-eddy simulation modeling framework. The model is extended to include multispecies transport and diffusion and is coupled to an advanced low-dissipation numerical scheme. The simulations correspond to a series of experiments for which particle image velocimetry measurements of two velocity components were made within the cavity, as well as fuel concentration measurements. Results are presented and compared with experimental measurements and to simulations made using the improved delayed detached eddy simulation model. The current model is able to predict mean and fluctuating quantities in a manner more consistent with the experiment, suggesting potential improvement over more traditional hybrid models.
机译:使用新型动态混合雷诺平均Navier-Stokes /大涡流仿真建模框架对Mach 2实验超声速腔进行仿真。该模型被扩展为包括多物种迁移和扩散,并与先进的低耗散数值方案耦合。该模拟对应于一系列实验,为此,在腔体内进行了两个速度分量的粒子图像测速测量,以及燃料浓度测量。呈现结果,并将其与实验测量结果进行比较,并与使用改进的延迟分离涡流仿真模型进行的仿真进行比较。当前模型能够以与实验更加一致的方式预测均值和波动量,这表明与更传统的混合模型相比,潜在的改进。

著录项

  • 来源
    《Journal of propulsion and power》 |2016年第6期|1343-1352|共10页
  • 作者单位

    Air Force Research Laboratory, Wright-Patterson Air Force Base, Ohio 45433;

    Innovative Scientific Solutions, Inc., Dayton, Ohio 45459;

    Mississippi State University, Starkville, Mississippi 39759;

    Mississippi State University, Starkville, Mississippi 39759;

  • 收录信息
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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