1) separated vortex
分离涡
1.
Comparisons of a) the location of the vortex core, b) strength of separated vortex, c) pressure distribution on the surface, d) forces and moments, e) turbulence viscosity ratio with experimental results indicat that all three k-ε models can simulate the separa.
分别利用Launder-Spaldingk-ε模式、Shihk-ε模式和重整群(Renorma-lizationGroup)k-ε模式模拟了细长旋成体在超音速中等大攻角下的背风面分离流,从背风面分离涡的强度和位置、物面压力分布、集中力和力矩以及湍流粘性比等方面比较了三种模式的计算结果,并与已有的试验结果进行了对比。
2.
In order to consider the effect of separated vortex on lateral hydrodynamic forces acting on a yawing ship,this paper gives a new free surface condition which includes the effect of vortex and puts forward a new concept of “vortex factor”.
为了考虑分离涡对斜航船体水动力的影响,推导了计及分离涡影响的自由表面条件,由此提出“涡影响因子”这一概念,并论述了涡流场速度势和兴波扰动势的数值计算方法。
3.
This paper puts forward a new free surface condition taking account for the “effect factor of vortex” in order to study the effects of the separated vortex on maneuvering hydrodynamic forces.
为了探讨船体分离涡对船舶操纵运动水动力的影响,文中给出了计及“涡的影响因子”的自由表面条件。
2) separation vortex
分离涡
1.
The computed results show that if the ratio between blade local thickness and clearance highness is too large or too small, the separation vortex will generate difficultly, and under the condition of rotating hub the separation vortex in tip region will gene.
计算结果表明,叶片当地厚度与间隙高度之比过大过小的情形均不易形成叶顶分离涡,相比轮毂静止的情形,轮毂转动时较不易形成叶顶分离涡。
2.
Finite Volume method was used to solve the three dimensional Navier Stokes equations of ideal gas,and combine flux conservative patched method and B L turbulence model correction to study this problem,capturing fluid field informations such as separation vortex,shock wave,expansion wave.
用有限体积法求解三维完全气体的Navier-Stokes方程,并将通量守恒的分区计算方法和B-L湍流模型修正结合在一起,捕捉到了间断处的分离涡、激波、膨胀波等流场信
4) separated vortex field
分离涡场
1.
The measurements of the separated vortex field and forces for drag plate show that the nose up pitching moment is produced due to the large induced downwash angle from the separated vortices of drag plate at the tail.
在NH-2风洞中对某机放减速板产生较大抬头力矩的机理进行了研究,通过减速板分离涡场的测量和测力试验表明,抬头力矩主要是由减速板分离涡在平尾处产生较大的诱导下洗角所致,诱导下洗角沿机身轴线向后逐渐减小,减速板前移可以消除抬头力矩。
5) tip vortex separation
梢涡分离
6) eddy shedding
涡流分离
补充资料:分离式分离机
分子式:
分子量:
CAS号:
性质:又称分离机。根据操作原理分类的一类离心机。用以分离更小固体颗粒(小于5微米)的不同浓度的场合和分离乳浊液和细粒子悬浮液。常用的有管式高速离心机、室式分离机、碟式分离机等。
分子量:
CAS号:
性质:又称分离机。根据操作原理分类的一类离心机。用以分离更小固体颗粒(小于5微米)的不同浓度的场合和分离乳浊液和细粒子悬浮液。常用的有管式高速离心机、室式分离机、碟式分离机等。
说明:补充资料仅用于学习参考,请勿用于其它任何用途。
参考词条