首页 | 本学科首页   官方微博 | 高级检索  
文章检索
  按 检索   检索词:      
出版年份:   被引次数:   他引次数: 提示:输入*表示无穷大
  收费全文   4篇
  免费   0篇
  国内免费   1篇
航空   3篇
航天   2篇
  2021年   1篇
  2008年   1篇
  2007年   2篇
  1994年   1篇
排序方式: 共有5条查询结果,搜索用时 15 毫秒
1
1.
《堂吉珂德》是世界文学史上的一座丰碑。自创作之日起,对其解读异彩纷呈、历久弥新。文章从美学角度分析了堂吉珂德富于幻想的思想特征,探讨了幻想或想象之于生活和创作的伟大影响,认为堂吉珂德式的想象是艺术创作的不竭之源。  相似文献   
2.
本文介绍了线谱对(Linear Spectrum Pair,LSP)分析的基本原理及其在G.729中的应用,同时分析比较了LSP参数与常用的线性预测系数LPC的区别,仿真结果表明,LSP参数的抗干扰能力远比LPC系数的抗干扰能力强。  相似文献   
3.
Pair creation in relativistic double layers in shown to have consequences for the charge density in the double layer and the current flowing through it.  相似文献   
4.
本文介绍了线谱对(Linear Spectrum Pair,LSP)分析的基本原理及其在G.729中的应用,同时分析比较了LSP参数与常用的线性预测系数LPC的区别,仿真结果表明,LSP参数的抗干扰能力远比LPC系数的抗干扰能力强.  相似文献   
5.
The flow field in a typical inward-turning inlet was visualized using the Planar Laser Scattering (PLS) method in a shock tunnel with a nominal Mach number of 6. The opaque inlet, which is truncated at a series of sections, and the following transparent isolator, are combined to enable the optical access at different streamwise locations. The sequential PLS images provide a tomography-like flow visualization, which confirm the existence of streamwise Counter-rotating Vortex Pairs (CVPs) in both external and internal flow field of the inlet. Generation mechanisms of these CVPs are unraveled with the help of a numerical simulation, among which the cowl notch plays an important role in the generation of surface trailing CVPs along the centerline of the cowl. Moreover, the cowl shock sweeps the internal boundary layer towards the body side, which ultimately accumulates low-momentum flow on the body side in forms of a large CVP propagating downstream through the isolator. The CVPs formed in the shape-transition are responsible for the nonuniform flow field of the inward-turning inlet. This study indicates that the V-shaped cowl notch affects the downstream flow significantly and, therefore, should be examined thoroughly in practical applications.  相似文献   
1
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号