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首页> 外文期刊>Proceedings of the Institution of Mechanical Engineers >Two-dimensional simulation of circulation control turbine cascade
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Two-dimensional simulation of circulation control turbine cascade

机译:循环控制水轮机叶栅的二维模拟

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The application of Coanda effect to turbine was first studied in this article through two-dimensional numerical simulation of circulation control turbine cascades. The influence of the aerodynamic and geometric parameters, such as the supply pressure of jet, the slot height, the shape, and curvature of the Coanda surface, on the performance of the circulation control turbine cascade was investigated in detail. The results show that the circulation control turbine cascade can achieve and exceed the performance level of the original turbine cascade (the baseline) at the cost of an acceptable jet supply pressure. The aerodynamic performance of circulation control turbine cascades is largely determined by two critical factors: the velocity of jet and the curvature of the Coanda surface. Low magnitude of jet velocity and large curvature of Coanda surface near the jet exit would lead to a serious jet detachment that is generally responsible for less flow turning and high energy loss. The jet attachment to the Coanda surface with a large curvature can be obtained only when the jet speed is high enough. Also, at this time, circulation control turbine cascade can bring a large flow turning but also a high energy loss based on a modified definition of the energy loss coefficient.
机译:本文首先通过循环控制涡轮叶栅的二维数值模拟研究了柯恩达效应在涡轮机中的应用。详细研究了空气动力学和几何参数,例如射流的供应压力,槽高度,附壁表面的形状和曲率,对循环控制涡轮叶栅性能的影响。结果表明,以可接受的射流供应压力为代价,循环控制涡轮机叶栅可以达到并超过原始涡轮机叶栅的性能水平(基线)。循环控制涡轮叶栅的空气动力学性能在很大程度上取决于两个关键因素:射流速度和柯恩达表面的曲率。较低的射流速度和靠近射流出口的附壁表面的大曲率将导致严重的射流分离,这通常导致较少的流量转向和较高的能量损失。仅当射流速度足够高时,才可以将射流附着到具有较大曲率的柯恩达表面。而且,此时,基于能量损失系数的修改定义,循环控制涡轮机级联可以带来大的转向流量,但是也带来高的能量损失。

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