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CLOSED-LOOP ACTIVE FLOW CONTROL OF THE WAKE OF A COMPRESSOR BLADE BY TRAILING-EDGE BLOWING

机译:尾缘吹气对压缩机叶片尾流的闭环主动流控制

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This paper presents a closed-loop active flow control strategy to reduce the velocity deficit of the wake of a compressor stator blade. The unsteady stator-rotor interaction, caused by the incoming stator wakes, generates fast changes of the rotor blade loading, affecting the stability and the performance of the overall compressor. Negative effects will be seen likewise when unsteady combustion concepts, such as a pulsed detonation, produce upstream disturbances. Furthermore, the periodic unsteady flow leads to additional undesired effects such as noise and blade vibrations. A controlled reliable manipulation of the stator wake is a way to handle these issues. Therefore, investigations on wake manipulation with trailing-edge blowing were carried out on a new low-speed cascade test rig. Detailed information about the wake profile is obtained by five-hole probe measurements in a plane downstream of the cascade for the natural and the actuated flow at a Reynolds number of 6×10~5. These measurements show a significant reduction of the wake velocity deficit for the investigated actuator geometry with an injection mass flow of less than 1% of the passage mass flow. Based on these results a position in the wake was chosen which is representative for the actuation impact on the velocity deficit. There, a hot-wire-probe measurement serves as the controlled variable. A family of linear dynamic black-box models was identified from experimental data to account for nonlinear and unmodelled effects. Static nonlinearitiy was compensated for by a Hammerstein model to reduce the model uncertainty and get a higher controller performance. To handle off-design conditions, a robust controller working in a range of Reynolds numbers from 5×10~5 to 7×10~5 was synthesized. The task of the controller is to rapidly regulate the controlled variable to a reference velocity by changing the blowing amplitude. The synthesized robust controller was successfully tested in closed-loop experiments with good results in reference tracking for pulse series up to 20 Hz. This translates into a much higher frequency when scaled to the dimension of a real machine.
机译:本文提出了一种闭环主动流控制策略,以减少压缩机定子叶片尾流的速度赤字。由传入的定子尾流引起的不稳定的定子-转子相互作用会导致转子叶片负载的快速变化,从而影响整个压缩机的稳定性和性能。当不稳定的燃烧概念(例如脉冲爆震)产生上游干扰时,也会产生负面影响。此外,周期性的不稳定流动会导致额外的不良影响,例如噪音和叶片振动。定子尾流的受控可靠操纵是解决这些问题的一种方法。因此,在新的低速级联试验台上进行了带有后缘吹气的尾流操纵的研究。有关尾流剖面的详细信息,可通过在级联下游的平面上对自然和驱动流的雷诺数为6×10〜5进行五孔探针测量获得。这些测量结果表明,对于所研究的执行器几何形状,尾流速度不足明显降低,而喷射质量流量小于通道质量流量的1%。基于这些结果,选择了尾流中的位置,该位置代表了对速度不足的致动影响。在那里,热线探针测量用作控制变量。从实验数据中确定了一系列线性动态黑匣子模型,以说明非线性和非模型效应。通过Hammerstein模型来补偿静态非线性,以减少模型的不确定性并获得更高的控制器性能。为了处理非设计条件,合成了一个鲁棒控制器,该控制器工作在雷诺数从5×10〜5到7×10〜5的范围内。控制器的任务是通过改变鼓风幅度将控制变量快速调节至参考速度。合成的鲁棒控制器已在闭环实验中成功测试,在高达20 Hz的脉冲序列参考跟踪中取得了良好的结果。当缩放到实际机器的尺寸时,这将转化为更高的频率。

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