1、

Numerical Simulation Study on Multistage Compressor Performance with Changing Tip Clearance

叶顶间隙变化对多级压气机性能影响的数值研究

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3、

Analysis about Three Dimensional Flow Field in a Multistage Compressor

某型多级压气机三维流场分析

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4、

To investigate the forcing function effects on the fundamental 2 E gust unsteady aerodynamic response of a multistage turbomachine blade row, a series of fundamental experiments are performed in an axial flow research compressor.

为了研究扰动力函数对多级叶轮机叶片排中基本的高、低能阵发非定常气动响应的影响,在研究用轴流压气机上进行了一系列的基础研究。

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5、

The effects of momentum and energy transportation caused by circumferential non uniformities of the flow in a multistage axial compressor are studied.

本文研究轴流压气机流场周向非均匀性的动量输运和能量输运作用。

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6、

meanwhile, a design method on the axial position of the stage with treated casing in multistage axial-flow compressors, i.e., the stage with maximum stalling pressure-rise capability would be treated, was suggested on the basis of much data from the compressor test rig.

在详细分析双级压气机实验数据的基础上,本文建议将多级轴流压气机处理级置于分级极限负荷最大的级上,这一新颖的机匣处理设计思路,受到了现有实验数据的支持。

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7、

Through flow numerical calculations including influence of spanwise mixing in a multistage axial flow compressor

计及气流展向掺混影响多级轴流压气机通流数值计算

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