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1)  steady flow
定常流
1.
Methods: The steady flow model and the pulsating flow model in the ductworkin vitrowere established.
方法:建立体外管道系统液体的定常流和脉动流模型,改变体流动速度探查导丝上两热电偶探头间距及管道内液体流动速度,用温度变化感应法测定并计算液体流动速度,所得数据与电磁流量计测得的平均速度进行相关性比较。
2.
The number and distribution of the singular points of streamlines in the cross section of steady flow through a curved tube are discussed by using the method of topological structure analysis.
利用拓扑结构分析方法 ,分析了弯曲圆管内定常流在横截面上流线的奇点个数及分布规律 ,给出了二次流的漩涡数目由 2个变为 4个 ,流态结构发生分叉现象的理论判据· 进而 ,利用Galerkin方法 ,得到了弯曲圆管内定常流的流函数和轴向速度的半解析表达式 ,给出了流态结构发生分叉现象的临界Dean数 ,所得结果与理论判则一
3.
It is showed by Galilean transformation of Euler’s formula that the flow type offluid will be different in different reference systems.As Bernoulli’s equation is valid only inreference systems in which ideal fluid flows in steady flow type,it is important to select aproper inertiai reference system in dealing with hydrodynamics problems such as Magnus ef-fect.
由于伯努利方程只适用于理想流体在其中作定常流的惯性系,从而说明在诸如马格努斯效应等流体动力学问题中选择合适惯性系的重要性。
2)  unsteady flow
非定常流
1.
Pressure gradient of unsteady flow of fluid in eccentric annulus with the inner cylinder reciprocating axially;
流体在内管做轴向往复运动偏心环空中非定常流的压力梯度
2.
Flow rate distribution of the unsteady flow of power law fluid in eccentric annuli with the inner cylinder reciprocating axially;
幂律流体在内管做轴向往复运动的偏心环空中非定常流的流量分布
3.
Numerical simulation of unsteady flow around propeller and rudder with additional thrust fin;
定常流中桨后舵附推力鳍的数值模拟
3)  steady flow
定常流动
1.
Applying the law of conservation of mass,movement theorem of steady flow, and applying the mathematical method of stream function with the consideration of the axis symmetry,the three components of velocity quantum of the flow are deduced in detail.
本文详细阐述了旋风分离器内流动在球坐标系中的数学表述和结果,应用质量守恒定律和定常流动的运动定律,在轴对称的考虑下,用流函数方法详尽推导了流动的三个速度分量。
2.
A method of semi-false transient to compute three dimensional steady flow was presented.
本文提出一种计算三维定常流动的半人工瞬变法,本方法的特点是直接利用流体力学的原始基本方程组进行数值计算。
4)  quasi-steady flow
准定常流
1.
On the hypothesis of isentropic flow and quasi-steady flow,a model of gas parameters in the storage chamber is established by a method of the lumped parameters.
在等熵流和准定常流假设条件下,采用集总参量法,建立了弹后高压火药气体通过小孔在弹体内气室与弹后空间之间流动的气体参数理论计算模型。
5)  unsteady flows
非定常流
6)  Steady airflow
定常气流
补充资料:定常流
稳定流。
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