Unsteady loss analyses of the flow in single-stage transonic compressor

单级 跨音速压气机内流场的非定常模拟及损失分析

The Numerical Optimization Design of Stacking Line at the Rotor 's Leading Edge of Transonic Compressor

跨 声速压气机转子前缘积叠线的数值优化设计

Calculation of Transonic Unsteady Flow Using Dynamic Unstructured Grids

基于非结构动网格的 跨 声速非定常流场求解

This configuration will provide good sustained supersonic cruise performance with a suitable engine type and good manoeuvre performance in transonic and supersonic regimes .

此配置将提供良好的用适当的引擎类型的持续超音速巡航性能，并在 跨音速和超音速操纵性能好制度。

A Static Aeroelastic Numerical Analytic Method of Transonic Flow About Wings

跨 声速机翼静气动弹性数值分析方法

Numerical investigation of flow field in a 1.5-stage transonic compressor

1.5级 跨音速压气机内部流场数值分析

An aerodynamic shape optimization of transonic wing design method for aeroelastic system

一种计及静气动弹性变形影响的 跨 声速机翼气动优化设计方法研究

The identification technology of unsteady aerodynamic loads shows a high efficient and accuracy approach for transonic aeroelastic solving .

证明非定常气动力辨识技术可以提供高效的高精度的气 动弹性分析。

Application of the Improved EGO Algorithm in Transonic Airfoil Aerodynamic Optimization Design

改进EGO算法在 跨 声速翼型气动优化设计中的应用

Empirical results are needed in the transonic Mach regime .

在 跨音速马赫数范围内需要经验结果。

Traditional gust responses are mainly analyzed based on linear aerodynamic load calculations in frequency-domain which is unsuitable for and the viscous and transonic flows .

传统的阵风响应主要在频域内进行分析，气动载荷基于线性方法计算，不能考虑黏性和 跨 声速流动影响。

Simulation of Transonic Unsteady Flow with Improved Unstructured Dynamic Grid Method

用改进非结构动网格方法模拟 跨音速非定常 绕流

A time-accurate three-dimensional Navier-Stokes solver of the unsteady flow field in a transonic fan was carried out .

采用全流道非定常数值模拟方法对进口稳态总压畸变条件下 跨 声速风扇流场进行求解。

The shock structure in a transonic compressor with the low aspect ratio of blading is three dimensional .

在低展弦比、低轮毂比的轴 流 压气机中激波结构常常是三维的。

The aerodynamic force is solved with the second order approximation method for transonic small disturbance potential flow .

跨音速和超音速空气动力学用 跨音速小扰动势流的二级近似方法求解气动力；

Effect of exciting frequency of casing treatment on transonic compressor performances

处理机匣激励频率对 跨 声速压气机性能的影响

The paper presents some research works on the internal flow shock wave measurement of transonic compressor by PIV technique .

在 跨 音压气机试验台上进行了用PIV技术测量内流激波结构的试验研究。

A novel vortex identification method for the visualization of the flow field is used for the study of the stall process of a transonic compressor .

通过将该方法与传统的动压头和流线、速度矢量等分析方法的结合，本文对所研究的 跨音速压气机的失速过程进行了分析和讨论。

Flapping and rotary gap have been investigated with the help of transonic unsteady aerodynamic forces .

使用 跨音速非定常空气动力，对扑动间隙和旋转间隙进行研究。

The aerodynamic performance computation of wings using transonic full potential equation

跨音速全位势方程的机翼气动性能计算

The Study on the Multi-objective Optimization Design of the Rotor of Transonic Compressor

跨 声速压气机转子多目标气动优化设计研究

Numerical Research on the Unsteady Flow and Loss in the Transonic Compressor

跨 声速压气机非定常流动及损失的数值研究

Influences of hub design on rotor performance in transonic compressor

轮毂曲线对 跨 声速压气机转子性能的影响

Research of Second Throat Design of Continuous Transonic / Supersonic Wind Tunnel

连续式 跨 声速风洞第二喉道设计技术研究

Research on flow instability mechanism of transonic compressor at low Reynolds number

跨 声速压气机低雷诺数下流动失稳机制研究

Effect of bowed and swept rotors on the unsteady efficiency fluctuation of a transonic compressor

动叶弯和掠对 压气机效率非定常波动的影响

With Time-Accurate simulation about one transonic fan stage unsteady flow some sketches related to unsteady flow are understood .

文章通过对一 跨 音风扇级非定常流场时间精确模拟，对叶轮机非定常流动建立了一定理解。

Partial structure similarity method to design composite transonic flutter model

一种复合材料 跨 声速颤振模型的部分结构相似设计方法

Research of data process methods and model excitation for transonic flutter experiments in wind tunnel

跨 声速风洞颤振试验模型激振与数据处理方法研究