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对当前跨音风扇气动设计体系中损失系数和堵塞系数的关联分析
引用本文:邢秀清,周盛,张健.对当前跨音风扇气动设计体系中损失系数和堵塞系数的关联分析[J].航空动力学报,1999,14(1):1-6.
作者姓名:邢秀清  周盛  张健
作者单位:1.National Laboratory of Aeroengine Aerodynamics & Thermodynamics, BUAA, Beijing 100083
摘    要:现有设计体系中对于损失系数主要是由实验和经验来确定。通流气动设计需计入叶片槽道内的附面层堵塞,反映附面层堵塞影响的堵塞系数也是依经验给定。本文对多台风扇设计进行分析后,发现现有的设计体系中损失系数和附面层堵塞系数之间彼此孤立,且不够协调,而事实上,两者是紧密相关的,体现在物理上就是损失和开式分离流之间的关系。本文在分析现有设计体系模型的基础上,提出了一个新的工程模型,把两者关联了起来,并给出了算例分析,且从算例结果中可以看到现有设计体系中单转子效率远大于级效率的原因之一。 

关 键 词:跨音速    风扇    叶栅    气动特性    分离流动    损失系数
收稿时间:4/1/1998 12:00:00 AM
修稿时间:1998年4月

CONNECTION BETWEEN LOSS COEFFICIENT AND BLOCK COEFFICIENT USED IN TRANSONIC FAN DESIGN
Xing Xiuqing,Zhou Sheng and Zhang Jian.CONNECTION BETWEEN LOSS COEFFICIENT AND BLOCK COEFFICIENT USED IN TRANSONIC FAN DESIGN[J].Journal of Aerospace Power,1999,14(1):1-6.
Authors:Xing Xiuqing  Zhou Sheng and Zhang Jian
Institution:1.National Laboratory of Aeroengine Aerodynamics & Thermodynamics, BUAA, Beijing 1000832.Gas Turbine Establishment Jiangyou Sichuan 621703
Abstract:Loss coefficient and block coefficient are interrelated in fact and the relation between them represents the relation between loss and separation.An engineering model is established to connect them,based on an analysis of many fan designs.The model determines the block coefficient from the loss coefficient,because the block coefficient derived from test loss coefficient is more believable than that from experience.At the same time,a computation test of a transonic fan is given as an example to verify the feasibility of the model.A conclusion has been drawn from the computation results that this model can estimate exactly the block coefficient and flow direction at the trail edge of rotor so as to improve the situation of the stator.It also explains why the rotor efficiency is superior to the stage efficiency.
Keywords:Transonic  Fan cascades  Aerodynamic characteristics  Separated flow  Loss coefficients  
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