论文标题
截短的理想情况下的喷嘴中的喷气谐振
Jet resonance in truncated ideally contoured nozzle
论文作者
论文摘要
在理想的轮廓喷嘴中,有一个过度膨胀的喷气机具有色调行为。研究了流场以了解其起源并显示其如何修改侧载属性。壁压和射流速度场的时间和空间组织首先是基于在喷嘴内的压力探针和高速时间分辨的PIV速度场中的同步采集这两种壁压的同步采集,该壁压在平面截面中测量的隔离式PIV速度场,该侧面横断了Nougzz射击的射流射击。首先证明了外部喷射空气动力学和内壁压力场明显连接,但只有在此频率峰值下,首先是波动壁压力的第一个方位角模式与首个波动外部速度场之间出现了显着的连贯性。进行延迟的分离涡流模拟并根据实验结果进行验证,以便重现这种音调流动动力学。模拟数据的分析表明,在整个流动结构中,第一个方位期模式的音调流动行为确实在整个流动结构中都更为大,在这些过程结构中,上游和下游传播波都被证明是共存的,甚至在喷嘴退出的下游甚至很远。分析表明,这两个波在射流芯中都有支撑,并且在分离区域具有不可忽略的压力特征。在此音调频率下,波动压力场的光谱正确正交分解表明,侧向压力的性质和强度是由与上游和下游传播相干结构相关的共振指导的,这会施加冲击波网络以响应网络并调节无嘴嘴的内部表面上的压力水平。
An overexpanded jet in a truncated ideally contoured nozzle is found to feature a tonal behavior. The flow field is investigated to understand its origin and show how it modifies side-load properties. The temporal and spatial organization of wall pressure and jet velocity field are first experimentally characterized based on synchronized acquisition of both wall-pressure along rings of pressure probes located within the nozzle and high-rate time-resolved PIV velocity fields measured in a plane section crossing the jet downstream of the nozzle exit. The external jet aerodynamics and internal wall pressure field are first shown to be clearly linked, but only at this frequency peak for which a significant coherence emerges between first azimuthal mode of fluctuating wall pressure and first azimuthal mode of fluctuating external velocity field. A Delayed Detached Eddy Simulation is carried out and validated against experimental results in order to reproduce this tonal flow dynamics. The analysis of simulation data shows that the tonal flow behaviour of first azimuthal mode is indeed more largely felt within the whole flow structure where both upstream and downstream propagating waves are shown to co-exist, even far downstream of the nozzle exit. The analysis shows that both waves possess support in the jet core and have a non negligible pressure signature in the separated region. The Spectral Proper Orthogonal Decomposition of fluctuating pressure field at this tonal frequency reveals that the nature and intensity of lateral pressure forces is directed by the resonance related to the upstream- and downstream-propagating coherent structures, which imposes the shock-waves network to respond and modulate the pressure levels on the nozzle internal surface.