助手标题  
全文文献 工具书 数字 学术定义 翻译助手 学术趋势 更多
查询帮助
意见反馈
   supersonic sharp cone boundary layers 的翻译结果: 查询用时:0.007秒
图标索引 在分类学科中查询
所有学科
更多类别查询

图标索引 历史查询
 

supersonic sharp cone boundary layers
相关语句
  超音速尖锥边界层
     Numerical Investigation of the Evolution of Disturbances in Supersonic Sharp Cone Boundary Layers
     超音速尖锥边界层中扰动演化特征的数值研究
短句来源
     The spatial evolution of 2-D disturbances in supersonic sharp cone boundary layers was investigated by direct numerical simulation(DNS) in high order compact difference scheme.
     采用高精度紧致格式,对超音速尖锥边界层中二维扰动的空间演化,进行了直接数值模拟.
短句来源
  “supersonic sharp cone boundary layers”译为未确定词的双语例句
     Basing on the steady flow, the evolution of 2-D T-S disturbances in supersonic sharp cone boundary layers with the oncoming flow of Mach number 5.29 and semi-angle 10°was investigated by direct numerical simulation (DNS).
     本文对来流马赫数为5.29,半锥角为10度的超音速零攻角尖锥边界层,根据上述模型得到定常基本流,并在计算域的入口处引入二维T-S扰动波,对其空间演化进行了直接数值模拟,并研究了流场中是否会出现小激波,及出现的小激波对流场结构的影响。
短句来源
  相似匹配句对
     Numerical Investigation of the Evolution of Disturbances in Supersonic Sharp Cone Boundary Layers
     超音速尖锥边界层中扰动演化特征的数值研究
短句来源
     The spatial evolution of 2-D disturbances in supersonic sharp cone boundary layers was investigated by direct numerical simulation(DNS) in high order compact difference scheme.
     采用高精度紧致格式,对超音速尖锥边界层中二维扰动的空间演化,进行了直接数值模拟.
短句来源
     A Numerical Study of the Evolution of 2-D Disturbance in Supersonic Sharp Cone Boundary Layer with Zero Angle of Attrack
     零攻角尖锥边界层中二维扰动演化特征的数值研究
短句来源
     On Laminar Boundary Layers with Suction
     有吸除的层流边界层问题
短句来源
     Basing on the steady flow, the evolution of 2-D T-S disturbances in supersonic sharp cone boundary layers with the oncoming flow of Mach number 5.29 and semi-angle 10°was investigated by direct numerical simulation (DNS).
     本文对来流马赫数为5.29,半锥角为10度的超音速零攻角尖锥边界层,根据上述模型得到定常基本流,并在计算域的入口处引入二维T-S扰动波,对其空间演化进行了直接数值模拟,并研究了流场中是否会出现小激波,及出现的小激波对流场结构的影响。
短句来源
查询“supersonic sharp cone boundary layers”译词为用户自定义的双语例句

    我想查看译文中含有:的双语例句
例句
为了更好的帮助您理解掌握查询词或其译词在地道英语中的实际用法,我们为您准备了出自英文原文的大量英语例句,供您参考。
  supersonic sharp cone boundary layers
The spatial evolution of 2-D disturbances in supersonic sharp cone boundary layers was investigated by direct numerical simulation (DNS) in high order compact difference scheme.
      
Numerical investigation of evolution of disturbances in supersonic sharp cone boundary layers
      


The spatial evolution of 2-D disturbances in supersonic sharp cone boundary layers was investigated by direct numerical simulation(DNS) in high order compact difference scheme.The results obtained suggested that although the normal velocity in the sharp cone boundary layer is not small,the evolution of amplitude and phase for small amplitude disturbances would be well in accord with the results obtained by the linear stability theory(LST) which supposes the flow is parallel.The...

The spatial evolution of 2-D disturbances in supersonic sharp cone boundary layers was investigated by direct numerical simulation(DNS) in high order compact difference scheme.The results obtained suggested that although the normal velocity in the sharp cone boundary layer is not small,the evolution of amplitude and phase for small amplitude disturbances would be well in accord with the results obtained by the linear stability theory(LST) which supposes the flow is parallel.The evolution of some finite amplitude disturbances was also investigated,and the characteristic of the evolution was shown.And shocklets were also found when the amplitude of the disturbances over some value.

采用高精度紧致格式,对超音速尖锥边界层中二维扰动的空间演化,进行了直接数值模拟.结果表明,虽然尖锥边界层流动存在一定的锥面法向速度,但小扰动的幅值及相位的演化都与由平行流假设得到的线性理论结果吻合.还研究了有限幅值扰动的演化,给出了其演化规律.并在扰动幅值增长到一定值时,发现了小激波.

 
图标索引 相关查询

 


 
CNKI小工具
在英文学术搜索中查有关supersonic sharp cone boundary layers的内容
在知识搜索中查有关supersonic sharp cone boundary layers的内容
在数字搜索中查有关supersonic sharp cone boundary layers的内容
在概念知识元中查有关supersonic sharp cone boundary layers的内容
在学术趋势中查有关supersonic sharp cone boundary layers的内容
 
 

CNKI主页设CNKI翻译助手为主页 | 收藏CNKI翻译助手 | 广告服务 | 英文学术搜索
版权图标  2008 CNKI-中国知网
京ICP证040431号 互联网出版许可证 新出网证(京)字008号
北京市公安局海淀分局 备案号:110 1081725
版权图标 2008中国知网(cnki) 中国学术期刊(光盘版)电子杂志社