• Lots of time accurate simulations about cascade flow field with different axial gaps are made.

    对不同轴向间距叶栅流场进行了大量时间精确模拟。

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  • This method is successfully applied on criticizing the holographic infinite interference diagram of the supersonic cascade flow field.

    并将该方法成功地应用于超音速叶栅流场全息干涉图的判读。

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  • A cavitation bubble in a cascade not only changes the flow field of the cascade, but also makes it difficult to calculate the flow field because of its unknown shape.

    叶栅汽蚀绕流时所产生的汽穴不仅使流场发生了变化,而且其未知的形状使流场的求解变得十分困难。

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  • The flow field visualization of a straight HP turbine cascade is conducted in a large-scale low-speed open -loop cascade heat transfer wind tunnel.

    在大尺寸低速开式叶栅传热风洞中对一种高压涡轮导向叶栅中的流场进行了流动显示实验研究。

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  • The flow field of straight HP turbine cascade was investigated experimentally in a large-scale low-speed open-loop cascade heat transfer wind tunnel.

    本文在大尺寸低速开式叶栅传热风洞中对一种高压涡轮导向叶栅中的流场进行了实验研究。

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  • An inviscid-viscous interaction method based on the inviscid time marching computer code has been employed to calculate the transonic flow field of two dimensional cascade.

    二维跨音速叶栅流场的计算是在无粘时间相关法计算程序的基础上采用无粘-边界层迭代而得。

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  • The flow field and the temperature field in the turbine cascade were studied in view of experiment and computation.

    本文从实验和计算的角度对涡轮叶片中的流场、温度场耦合进行了研究。

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  • The effect of slot inlet Angle and turning Angle on flow field characteristic of cascade with slot was studied numerically.

    数值模拟了槽道进气角和转折角对开槽叶栅流场特性的影响。

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  • Because of relative movement of blade rows, the pressure distributions on the blade and the flow field in the cascade vary periodically.

    由于叶排间的相互运动,使叶片表面压力和叶栅通道内的流场呈周期性地变化;

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  • Finally, the dynamic response study analyzes rotor cascade under aerodynamic force with the steady state results of the flow field calculations.

    最后结合在不同转速下的流场稳态计算结果,对叶栅进行在气动力作用下动态响应分析。

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  • Steady flow fields are also calculated to analyze flow field structure for the same cascade with different inlet Mach Numbers and incidence Angle.

    对于同一叶栅进行了定常流场的计算与分析,比较了平面叶栅在不同进口马赫数、不同攻角下的定常流场。

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  • The detailed flow field of ejection cascade was obtained by using a compact ejection model coupled with the calculation of main flow field.

    应用一维源项喷气模型,结合涡轮叶栅流场数值模拟,得到了不同喷气形式下涡轮叶栅流场细节。

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  • After optimization, the flow field in cascade passage is effectively improved, and the performance of stage is improved obviously.

    对比数值模拟结果,优化后有效地改善了叶栅流道中的流动状况,级性能有了显著的提高。

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  • In the calculation of flow field in 2-d transonic cascade, wave has been exactly captured and results are satisfactory.

    在平面叶栅跨音流场的计算中,较好地捕获了激波,与实验比较,结果令人满意。

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  • The flow visualization by means of smoke and measurement of 3 -d flow field are conducted to investigate physical model of the streamwise corner vortexes in a compressor cascade.

    本文采用烟显示和三维流场测量的方法,研究扩压叶栅角涡的物理模式。

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  • The flow visualization by means of smoke and measurement of 3 -d flow field are conducted to investigate physical model of the streamwise corner vortexes in a compressor cascade.

    本文采用烟显示和三维流场测量的方法,研究扩压叶栅角涡的物理模式。

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