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CAVITATION FLOW STRUCTURE AND UNSTEADY PRESSURE PULSATION AROUND A HYDROFOIL

机译:水翼周围的空化流结构和非定常压力脉动

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The present work is an original study of the flow induced vibration, cavitation structures and cavitation induced pressure pulsation characteristics around a typical hydrofoil named 791, which is widely applied in the axial flow pump. From the vibration experiment of the hydrofoil at various operating conditions, it is clear that at low frequency band, with Reynolds number increasing, vibration energy first experiences a stable slightly increasing tendency, and then decreases rapidly, finally rises steeply again. Besides, according to the results of several positive incidence angles, it is observed that vibration energy usually achieves a local minimum level at a certain positive incidence angle falling into the range of 2° to 4°. Based on results obtained from the detached eddy simulation (DES) turbulent model, full developing process of cavitation stages including, incipient cavitation, sheet cavitation and cloud cavitation could be captured and easily identified. It is found that pressure spectra in accordance with different cavitation stages show great discrepancy. In the stage of incipient cavitation and cloud cavitation, predominant components in pressure spectra are caused by the cyclical evolution of the main cavity and the periodic variation of the small vacuoles shedding at the span-wise outer edge of the hydrofoil. However, in sheet cavitation stage, the pronounced excitation frequencies are generated by cyclical evolution of the main cavity and cavity shedding from both sides of the U-shaped cavitation structure. Pressure pulsation amplitude is pretty small at the cavity stable adhesion region. But the amplitude of vacuoles shedding from the hydrofoil is much larger than main cavity adhesion region at these three stages.
机译:目前的工作是对典型的称为791的水翼的水流引起的振动,空化结构和空化引起的压力脉动特性的原始研究,该水翼被广泛地应用于轴流泵中。从水翼在各种工况下的振动实验可以清楚地看出,在低频段,随着雷诺数的增加,振动能量首先经历了稳定的略微增加的趋势,然后迅速减小,最后又陡然上升。此外,根据几个正入射角的结果,观察到振动能量通常在一定的正入射角落入2°至4°范围内时达到局部最小水平。根据从分离涡模拟(DES)湍流模型获得的结果,可以捕获并轻松识别空化阶段的完整开发过程,包括初期空化,片状空化和云空化。发现根据空化阶段的压力谱显示出很大的差异。在初生空化和云空化阶段,压力谱中的主要成分是由主腔的周期性演变和小翼空泡在翼型的翼展方向外缘脱落的周期性变化引起的。但是,在薄板空化阶段,通过U型空化结构两侧的主腔和空洞的周期性演化而产生明显的激发频率。在空腔稳定的粘附区域,压力脉动幅度很小。但是在这三个阶段中,从水翼上脱落的液泡的幅度远大于主腔粘附区。

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