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
共[254]条 当前为第1条到20条[由于搜索限制,当前仅支持显示前5页数据]
 

相关语句
trailing edge
The magnitude of this flow circulation is determined from the condition under which the flow leaves the trailing edge of the body (the analog of the Chaplygin-Zhukovskii postulate in potential flow).
      
We solve the problem of the natural oscillations of a gas flowing past a cascade of flat plates under the Joukowsky-Chaplygin condition that the velocity at the trailing edge of the profiles is finite.
      
The formation of a laminar wake in the flow behind a shock wave when the latter is shed from the trailing edge of a semi-infinite plate is investigated in this paper.
      
An analytic solution of the problem of the wake in the neighborhood of the trailing edge is obtained, from which it follows that, in contrast to [2], there is no line of singularities in the nonstationary boundary-layer equations in the flow domain.
      
This fact is also verified by the analysis of the flow in the neighborhood of a line of tagged particles leaving the trailing edge simultaneously with the shock wave.
      
The part of the edge of the lifting surface from which the wake vortex surface is shed is called the trailing edge.
      
A characteristic feature of flows of this type is the influence of the conditions specified on the trailing edge of the body on the complete upstream flow field [3-5].
      
As in [8, 9], the solution is obtained analytically in the form of universal formulas applicable for any pressure specified on the trailing edge of the plate.
      
The obtained solutions therefore contain no information about the influence of the trailing edge of the wing, on which, as is well known, the Chaplygin-Zhukovskii condition is satisfied.
      
The influence of the change in the pressure on the trailing edge of the plate on the boundary layer characteristics is investigated.
      
Flow in the neighborhood of the trailing edge of a plate in a transonic flow of viscous gas
      
An investigation is made into the influence of the Mach number and the viscosity on the flow in the neighborhood of the trailing edge of a plate.
      
Turbulent flow of a fluid in the neighborhood of the trailing edge of a plate at zero angle of attack
      
The laminar flow regime of an incompressible fluid at the trailing edge of a plate was studied by Stewartson and Messiter [1, 2] by means of the method of matched asymptotic expansions.
      
Solution of Navier-Stokes equations near the trailing edge of a plate
      
Structure of the flow of a viscous gas near the trailing edge of a flat plate
      
Solution of the complete system of Navier-Stokes equations forms the basis for a study of the nature of flow of a viscous heat-conducting gas in the neighborhood of a trailing edge of a flat plate.
      
As a result the flow upstream near the trailing edge of the plate will depend on the flow immediately behind the edge, since the perturbations propagate both upstream and downstream in this case.
      
Contribution to the theory of thin-profile trailing edge separation
      
The conditions of nonsymmetric trailing edge flow with separation are investigated.
      
 

首页上一页12345下一页尾页 

 
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