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NUMERICAL SIMULATION OF A HIGHLY LOADED LPT CASCADE WITH STRONG SUCTION SIDE SEPARATION UNDER PERIODICALLY UNSTEADY INFLOW CONDITIONS

机译:周期性流入条件下具有强力吸力侧分离的高负载LPT级联的数值模拟

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The effects of periodically unsteady inflow conditions on boundary layer development of a highly loaded low pressure turbine cascade have numerically been studied using an unsteady Reynolds averaged Navier-Stokes solver. The numerical results show good agreement with measurement data by means of time mean profile pressure distribution and unsteady boundary layer development. In particular a reduction of the suction side separation bubble caused by the wakes is well reproduced. For increasing wake passing frequencies this reduction becomes even more pronounced. An independent variation of the flow coefficient reveals that the trajectory of the wake through the blade passage is influenced and velocity disturbances induced by the wake interact more strongly with the boundary layer on the blade as the flow coefficient decreases.
机译:定期不稳定流入条件对高负载低压涡轮机级联的边界层开发的影响,使用了一个不稳定的雷诺斯平均的Navier-Stokes求解器进行了数量的研究。数值结果通过时间平均曲线压力分布和不稳定的边界层开发显示了与测量数据的良好一致性。特别地,由唤醒引起的吸入侧分离气泡的减小很好地再现。对于增加唤醒传递频率,这种减少变得更加明显。流量系数的独立变化揭示了通过叶片通道的锯齿的轨迹是由爪子的影响和速度干扰在流量系数减小时与刀片上的边界层更强烈地相互作用。

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