首页> 外文会议>Proceedings of the 2002 ASME Joint U.S.-European Fluids Engineering Conference >PARAMETRIC STUDY OF THE DISCHARGE COEFFICIENT ON CRITICAL SONIC NOZZLES ISO-9300 WITH TURBULENT BOUNDARY LAYER
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PARAMETRIC STUDY OF THE DISCHARGE COEFFICIENT ON CRITICAL SONIC NOZZLES ISO-9300 WITH TURBULENT BOUNDARY LAYER

机译:湍流边界层临界声波喷嘴ISO-9300放电系数的参数研究

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A parametric study on determining discharge coefficient in ISO 9300 toroidal sonic nozzles have been developed. The focus of this paper is to obtain the an analytical model for the calculus of this discharge coefficient on turbulent boundary layer conditions for gases at Pr=0.7. The problem is divided in two sections: one in which the viscous stresses are taking in to account at boundary layer zone, based on turbulent boundary layer theory and taking as starting point the work carried out by Stratford. Then, curvature of flow field is studied at the nucleus of the nozzle, obtaining discharge coefficient values using numerical simulation for a two-dimensional flow. The results have a good agreement with correlations of ISO-9300 ,experimental and numerical data of Wu-Yan and the analytical model from Stratford.
机译:已经进行了确定ISO 9300环形声波喷嘴中的排放系数的参数研究。本文的重点是获得在Pr = 0.7时气体在湍流边界层条件下该排放系数演算的解析模型。该问题分为两部分:一是基于湍流边界层理论,以斯特拉特福德所做的工作为出发点,其中在边界层区域考虑了粘性应力。然后,在喷嘴的原子核处研究流场的曲率,使用二维流动的数值模拟来获得排放系数值。结果与ISO-9300的相关性,吴岩的实验和数值数据以及斯特拉特福德的分析模型具有良好的一致性。

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