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Unsteady Characteristics of Resonant Supersonic Dual Impinging Jets

机译:超声速双撞击射流的非定常特性

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Supersonic single impinging jet flows are well studied and are known to exhibit strong unsteadiness levels, especially when resonance dominates. However, much less is known about the unsteady characteristics of two such jets operating in tandem, such as those in the F-35B aircraft, where flow unsteadiness is also influenced by jet-jet interaction and coupling. Therefore, flow-field associated with a pair of identical underexpanded jets at Nozzle Pressure Ratio (NPR) 2.65, discharged from identical converging nozzles with exit diameters 25.4 mm each, and impinging normal to a surface is investigated. Comparisons are made with a single impinging jet operated at identical conditions by contrasting the features seen in shadowgraph flow visualization, nearfield acoustics and surface pressure measurements on the ground plane. Strong unsteadiness levels, feedback mechanism that drives resonance and the corresponding instability mode shapes, are some of the similarities seen between the single and dual impinging jet configurations. Increased low frequency unsteadiness and a substantial reduction in the strength of axisymmetric instability modes in the case of dual impinging jets are also observed. Further, the fountain flow generated between the two jets is found to play an important role in affecting the unsteady characteristics in dual impinging jets.
机译:对超音速单次冲击射流进行了充分的研究,并已知表现出很强的不稳定度,尤其是在共振占主导的情况下。但是,对于两个串联运行的喷气机(例如F-35B飞机)的不稳定特性了解得很少,在这种情况下,流量不稳定还受到喷气机相互作用和耦合的影响。因此,研究了与在喷嘴压力比(NPR)为2.65时从一对相同的会聚喷嘴(每个出口直径为25.4 mm)排放的,垂直于表面撞击的一对相同的膨胀不足喷嘴相关的流场。通过对比在阴影图流动可视化,近场声学和地面上的表面压力测量中看到的特征,对在相同条件下运行的单个撞击射流进行了比较。强烈的不稳定状态,驱动共振的反馈机制以及相应的不稳定性模式形状,是单次和双次撞击射流配置之间的一些相似之处。在双撞击射流的情况下,还观察到增加的低频不稳定性和轴对称不稳定性模式强度的显着降低。此外,发现在两个射流之间产生的喷泉流在影响双撞击射流的不稳定特性方面起着重要作用。

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