首页> 外文期刊>Journal of Applied Mechanics and Technical Physics >NUMERICAL SIMULATION OF INSTABILITY DEVELOPMENT AT THE CONTACT BOUNDARIES IN A THREE-LAYER GAS SYSTEM: COMPARISON WITH EXPERIMENTAL DATA
【24h】

NUMERICAL SIMULATION OF INSTABILITY DEVELOPMENT AT THE CONTACT BOUNDARIES IN A THREE-LAYER GAS SYSTEM: COMPARISON WITH EXPERIMENTAL DATA

机译:三层气体系统联络边界处不稳定发育的数值模拟:与实验数据的比较

获取原文
获取原文并翻译 | 示例
           

摘要

This paper presents the results of experimental and computational studies of instability development and mixing at the contact boundaries between gases of different densities. It has been shown that instability and mixing at two contact boundaries in a three-layer gas systems occur after a shock wave with a Mach number M = 1.3 that forms on the left end and moves along the tube has passed through the contact boundaries. Two experiments were performed, in the first of which the central layer was filled with a heavy gas (SF6 gas), and in the second experiment, it was filled with a light gas (helium). On the left and right of the central layer was air at atmospheric pressure. A comparison of the results was performed.
机译:本文介绍了不稳定开发的实验和计算研究的结果,并在不同密度气体之间的接触边界处混合。 已经表明,在带马赫数M = 1.3的冲击波之后发生在三层气体系统中的两个接触边界处的不稳定性和混合在左端形成并且沿着管移动已经通过接触边界。 进行两个实验,在第一实验中,中央层填充重气(SF6气体),并在第二实验中填充有轻气(氦气)。 在中心层的左侧和右侧是气压的空气。 进行结果进行了比较。

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