首页> 外文会议>ASME/JSME Fluids Engineering and Laser Anemometry Conference and Exgibition >EXPERIMENTAL AND THEORETICAL STUDY OF THE 2-D BLADE LIFT ALTERATION BY TRAVELING BUBBLE CAVITATION
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EXPERIMENTAL AND THEORETICAL STUDY OF THE 2-D BLADE LIFT ALTERATION BY TRAVELING BUBBLE CAVITATION

机译:泡沫空化2-D叶片升降改变的实验与理论研究

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The setting level of a hydraulic machine, specially for low head turbines, is decided with respect to the possible alteration of the efficiency due to the cavitation development. Observation of the cavity extent in the flow passage of the runner allows to associate the drop in efficiency with a particular type of cavity development. However, depending on the type of cavities, this efficiency loss can not be very easily explained. Obviously, for a cavity attached to the leading edge of the blade, the presence of the vapor phase on the blade suction side limits the pressure at the vapor tensile strength value. In the case of traveling bubble cavitation, corresponding to the Francis turbines outlet cavitation at the nominal head, an experiment with a 2-D NACA profile shows that the modification of the mean pressure field is mainly due to the bubble dynamics. The measured evolution of the bubble radius along the blade allows to compute the pressure field around the bubble as a function of time. It allows to correct the pressure coefficient distribution without cavitation adding the pressure field generated by the bubbles expressed in term of mean pressure coefficient. This correction depends on the nuclei radius distribution. Thus, the aim of the paper is to present the results and the analysis of an experiment intending to explain the influence of the nuclei content on this mean pressure field modification due to the bubble dynamics on a 2D profile. A modelisation of the influence of the bubble dynamics on the mean pressure field is also undertaken, whose results are compared to the measurements.
机译:特别是用于低头涡轮机的液压机的设定电平,决定了由于空化发育而效率的可能改变。观察流道的流动通道中的腔体程度允许将降低效率与特定类型的腔显影相关联。然而,取决于腔的类型,这种效率损失不能很容易解释。显然,对于附着到刀片的前缘的腔,叶片吸入侧的气相的存在限制了蒸汽拉伸强度值的压力。在行驶气泡空化的情况下,对应于标称头部的母频涡轮机出口空化,具有2-D Naca曲线的实验表明,平均压力场的变形例主要是由于气泡动力学。沿着刀片的气泡半径的测量演变允许以时间的函数计算气泡周围的压力场。它允许校正压力系数分布而不进行空化添加由平均压力系数期间表示的气泡产生的压力场。该校正取决于核半径分布。因此,本文的目的是呈现出于2D轮廓上的气泡动力学而解释核含量对该平均压力场修改的实验的结果和分析。还进行了对泡沫动力学对平均压力场的影响的造型,其结果与测量相比。

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