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A pictorial analysis of jet and vortex behaviours during attack transients in organ pipe models

机译:器官管模型攻击瞬态期间射流和涡流行为的图形分析

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Attack transients in organ pipes are investigated by analyzing slow-motion pictures from the smoked-jet visualization with a high-speed digital video camera. In our experiment the attack is very slow and the 90% rise time of the blowing pressure is over 50 fundamental periods. Also, lower final blowing pressures (typically 150Pa) and longer cutup lengths (10.2 and 15.8 mm) are used. Although the jet issuing from the flue almost always deviates exteriorly, the jet impinging straight on the edge is incidentally observed. This head-on impinging jet is followed by two symmetrical forward-spinning vortices. The exteriorly-deviating jet is characterized by the type of the vortex formed during initial jet-edge interaction: (1) no vortex; (2) a forwardspinning vortex just beneath the edge; (3) an almost stationary vortex before the edge; (4) a backspinning vortex just beneath the edge (this example is borrowed from M. P. Verge ef al. [1], and is observed when a very fast attack is applied to a short pipe with a short cutup). A forwardspinning vortex seems to promote a smoother buildup of the jet wave; a backspinning vortex yields complicated interactions among the main jet flow, its side flow, the entrained flow, and the edge; a stationary vortex largely retards the jet-wave buildup by inducing the two-crest (hydrodynamically second) mode; two symmetrical vortices need reaction time to adapt themselves to asymmetrical sinuous disturbance along the jet. Also, a kind of subharmonic jet oscillation occurs during this transformation. The two-crest mode is followed by complicated transfigurations such as the three-crest mode before the ordinal one-crest mode is established. The presteady state just prior to the steady state is characterized by the acoustic vortex shedding from the edge surface, which however disappears at the steady state. [References: 15]
机译:通过使用高速数字摄像机分析烟熏喷射可视化中的慢动作图片,研究了器官管中的瞬态攻击。在我们的实验中,起音非常缓慢,吹气压力的90%上升时间超过了50个基本周期。同样,使用较低的最终吹制压力(通常为150Pa)和较长的切割长度(10.2和15.8 mm)。尽管从烟道射出的射流几乎总是向外偏移,但是偶然地观察到直接撞击在边缘上的射流。该正面撞击射流之后是两个对称的向前旋转涡流。向外偏离的射流的特征在于在初始射流-边缘相互作用期间形成的涡流的类型:(1)没有涡流; (2)边缘下方正向旋转的涡旋; (3)边缘之前几乎静止的涡旋; (4)边缘下方的反向旋转涡流(此示例是从M. P. Verge等人[1]借来的,当对具有短截距的短管施加非常快速的攻击时,可以观察到)。向前旋转的涡流似乎促进了喷射波的更平滑的积聚。逆旋涡在主射流,其旁流,夹带流和边缘之间产生复杂的相互作用。静止的涡流通过诱发两波峰(流体动力学第二模式)而大大阻碍了喷射波的形成;两个对称的涡流需要反应时间才能适应射流的不对称弯曲扰动。同样,在这种转换过程中会发生一种次谐波喷射振荡。在建立有序的单峰模式之前,两峰模式之后是复杂的变形,例如三峰模式。刚好在稳态之前的预稳态的特征在于,声学涡流从边缘表面脱落,但是在稳态时消失。 [参考:15]

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