基于多特征提取的合成射流涡流控制机理研究

STUDY ON VORTEX CONTROL MECHANISM OF SYNTHETIC JET BASED ON FEATURE EXTRACTION METHODS

  • 摘要: 在横流的底部施加倾斜角为60^\circ 的合成射流,并采用大涡模拟(LES)对其周期性涡运动过程进行了数值模拟,研究不同激励参数条件下合成射流与横流相互作用涡环结构的产生机理及演变规律。该文首先利用第三代涡识别方法(Liutex矢量法)对流场中涡环的演变过程进行了运动跟踪,并且定量统计合成射流在不同驱动频率( St = 0.25,0.5,0.75,1 )和驱动振幅(A_0 = 1,1.5,2,2.5)下涡旋结构的旋转强度和涡核尺度。此外,采用本征正交分解法(proper orthogonal decomposition, POD)方法和动态模态分解(dynamic mode decomposition, DMD)对合成射流特定频率(St = 0.25)及振幅(A_0 = 2.5)下流场速度场进行模态分解,提取影响流场的主特征模态。结果表明:振幅对旋转强度和涡核尺寸大小有正贡献,而频率对旋转强度和涡核尺寸大小有负贡献;合成射流在横流中的涡运动机理可以概括为,在低频低振幅条件下有利于顺时针涡结构的产生,而在高频高振幅条件下有利于逆时针涡结构的产生;基于各阶POD模态的空间结构及频谱特征等特性,流场主特征结构为脱落涡,脱落频率与射流驱动频率一致(St = 0.25)。初级顺时针涡旋结构为涡流控制的主导结构,而每阶模态均为多频耦合;通过DMD对流场信息进行时空解耦,得到了剪切诱导、涡合并等动力特征。多种特征提取方法的结合更有助于合成射流涡流控制机理的深入研究。

     

    Abstract: A synthetic jet with an inclination angle of 60 ° is applied at the bottom of a crossflow, and its periodic vortex motion is numerically simulated by large eddy simulation (LES). The generation and evolution mechanism of the vortex interaction between the synthetic jet and the cross flow are studied under different driving parameters. The third-generation vortex identification method (Liutex vector) is used to track the vortex evolution in the flow field. The rotation intensity and vortex core size of the vortex structure, which are generated by the synthetic jet under different driving frequencies (St=0.25, 0.5, 0.75, 1) and driving amplitudes (A0=1, 1.5, 2, 2.5), are quantitatively recorded. In addition, the proper orthogonal decomposition (POD) and dynamic mode decomposition (DMD) are used to extract the structure and frequency features of the flow field with specific frequency (St=0.25) and amplitude (A0=2.5) of the synthetic jet, and the main characteristic modes affecting the flow field are analyzed. The results show that amplitude has positive contribution to the rotation intensity and vortex core size, while frequency has negative contribution to the both. The vortex motion mechanism of synthetic jet in crossflow can be summarized as follows: under the condition of lower frequency and lower amplitude, the clockwise vortex structure is favorable, while it is beneficial to the generation of counter-clockwise vortex under higher frequency and higher amplitude. Based on the spatial structure and spectrum characteristics of POD mode, the main characteristic structure of the flow field is shedding vortex with a shedding frequency of St=0.25, which is consistent with the jet driving frequency. The primary clockwise vortex structure is found to be the dominant structure for jet vortex control, while each mode is multi-frequency coupling. The flow field information is decoupled in time and space by DMD, and the dynamic characteristics in terms of shear induction and vortex merging are captured. Therefore, the combination of various feature extraction methods contributes more to the profound study of the mechanism of vortex control of synthetic jet.

     

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