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湍流边界
1、boundary condition───边界条件，极限条件；[数]边界条件，界面条件
2、boundary rider───n.牧场巡修围栏工人
3、turbulent flow───[流]湍流；[流]紊流；湍流; 紊流; 溜
4、divergent boundary───[海洋][地质]离散边界
5、obed boundary───obed边界
6、collision boundary───碰撞边界
7、boundary───n.边界；范围；分界线
8、turbulent───adj.动荡的；湍流的；与紊流有关的
9、boundary line───边界线；疆界线；受恩的，义务的; 界线
1、A Mechanism for the Excitation of Coherent Structures in the Wall Region of a Turbulent Boundary La───湍流边界层外区扰动激发近壁区相干结构的一种机制
2、The problem on turbulent boundary layer in open-channel flow is an important element of turbulence research.───明渠紊流边界层问题是明渠紊流研究中的一项重要内容。
3、Turbulent boundary layers along two surface of curvature were investigated with computation.───本文计算了沿不同曲面流动的湍流边界层。
4、A dissipation integral method is developed for calcalating compressible turbulent boundary layers on planar bodies.───发展了二维可压湍流边界层的耗散积分方法。
5、The fourth chapter studies on the numerical simulation of an incompressible turbulent boundary flow on a plate.───第四章对不可压缩平板湍流边界层流动进行了计算。
6、An incompressible turbulent boundary layer separation in a two-dimensional diffuser was surveyed using laser doppler velocimeter .───用激光多普勒技术测量了二维扩压器中不可压湍流边界层分离流动，得到了时均速度和雷诺剪应力分布。
7、Finally recent studies of turbulent boundary layer separation are also briefly reviewed.───最后简单介绍了目前在研究湍流边界层分离方面的进展。
8、The method can be extended to axisymmetric and three-dimensional turbulent boundary layers if the pressure gradient effect is considered.───如果考虑压力梯度的影响，还可以将该方法推广到轴对称和三维湍流边界层中去。
9、Numerical results of steady, compressible, lamina and turbulent boundary layers over the finite swept wing show to be satisfactory.───算例表明，能获得令人满意的三维机翼定常可压缩层、湍流边界层的计算结果。
1、Three-dimensional turbulent boundary layer on the ground board is measured through the ground effect tests of a delta wing with aspect ratio 3.
2、The separating flow in a turbulent boundary layer was surveyed in a 2-D curved-wall diffuser by employing 2-D laser Doppler velometer.
3、A method is proposed to calculated the incompressible three-dimensional turbulent boundary layer on both wall surfaces of vaneless diffusers.
4、A dissipation integral method is developed for calcalating compressible turbulent boundary layers on planar bodies.
5、Two-dimensional incompressible turbulent boundary layer growth on the blades is calculated taking into account the blade surface curvature effect and also the rotational effect.
6、Viscous - flow, laminar and turbulent boundary layers.
7、The Two-Layer Model (TLM) differential method for turbulent boundary layers is rapidly developed over the last decade.
8、The measurement technique of constant temperature anemometry was used to study experimentally the mechanism of drag reduction in turbulent boundary layer with riblet surface.
9、It provides qualitative information mainly concerning the overall flow structure, such as the turbulent boundary layer separation, reattachment locations and the dimensionalities of the flow.