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Active Control of Jets in Crossflow

机译:错流中的射流主动控制

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摘要

The present study quantifies the dynamics of actuation for the temporally forced, round gas jet injected transversely into a crossflow, and incorporates these dynamics in developing a methodology for open loop jet control. A linear model for the dynamics of the forced jet actuation is used to develop a dynamic compensator for the actuator. When the compensator is applied, it allows the jet to be forced in a manner which results in a more precisely prescribed, temporally varying exit velocity whose RMS amplitude of perturbation can be made independent of the forcing frequency. Use of the compensator allows for straightforward comparisons among different conditions for jet excitation. Clear identification can be made of specific excitation frequencies and characteristic temporal pulse widths which optimize transverse jet penetration and spread through the formation of distinct, deeply-penetrating vortex structures. Further details on this work may be found in M'Closkey et al. (2002).
机译:本研究量化了横向注入到横流中的暂时受力的圆形气体射流的驱动动力学,并将这些动力学纳入开环射流控制方法的开发中。用于强制射流致动动力学的线性模型用于开发致动器的动态补偿器。当应用补偿器时,它可以使射流受力,从而产生更精确规定的随时间变化的出口速度,其摄动RMS幅度可以独立于强迫频率而定。补偿器的使用允许在喷射激励的不同条件之间进行直接比较。可以明确识别出特定的激发频率和特征性的时间脉冲宽度,这些脉冲宽度可以优化横向射流的穿透和扩散,形成独特的深穿透涡结构。关于这项工作的更多细节可以在M'Closkey等人的文章中找到。 (2002)。

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