回转流

任意回转流面上跨音速压气机叶栅含激波流场的计算

Calculation of shocked flow along a STREAM-SURFACE of revolution in transonic compressor cascade

任意回转流面叶栅出气角的确定

Predicting exit flow angle for flow past cascade section on an arbitrary stream surface of revolution

本文运用时间分裂有限体积法，进行了任意回转流面上跨音速压气机叶栅含激波流场的计算。

In the present paper , the time-split finite-volume method is successfully used to calculate shocked flow in transonic compressor cascade .

回转体流噪声相似律的实验研究

Experimental study of flow noise scaling of an axisymmetric body

转捩区长度对回转体流噪声的影响

Effect of length of the transition zone on the sound radiation from the boundary layer of an axisymmetric body

回转体空泡流特性研究散货物流信息集成

Research on characteristics of flow around cavitating body of revolution

本文采用二维不可压理想流动和湍流边界层的流动模型计算了多叶风机的内部流场，子午面和回转面的位流速度计算采用积分方法；

This article adopts the flow model of 2-D non-compressible ideal flowing and turbulent flowing boundary layer to compute the internal flow field for a multiblade fan , while potential flow speed for meridian plane and rotational plane uses integrated method ;

回转体空泡绕流现象的数值模拟

Phenomenon Numerical simulation of cavitation flow on revolution body

轴面流线分点计算计算回转体粘性绕流的流线迭代法

A Streamline Iteration Method for Calculating the Viscous Flows around Bodies of Revolution

不同肋间距变截面回转通道内的流阻和换热特性

Characteristic of Flow Resistance and Heat Transferin a Turnover Variable Cross-Section Channel with Different Rib Pitches

使用非正交曲线坐标与非正交速度分量的S1回转面跨声速流时间相关数值解

The time-dependent numerical solution of transonic flow on s_1 surface of revolution employing non-orthogonal curvilinear coordinates and non-orthogonal velocity components

基于势流理论和边界元方法，对水下运动的回转体的空泡流进行了数值模拟.将半经验空泡封闭模型由平面流动推广至轴对称流动。

Axisymmetric cavitating flows around the cone-capped cylinder are numerically simulated with the boundary element method under potential flow assumption .