摘要
同时采用标准k-ε及非线性k-ε模型在附体坐标系下求解定常不可压N-S方程组计算扩压器内湍流流场,得到了扩压器的压力恢复系数和速度分布,与实验结果对比发现非线性k-ε模型预测的结果更吻合实验值,且能测出临界扩压角下的局部分离流。文中着重研究了非对称扩压器,并给出了用两种模型计算的湍流量。
In order to solve steady N S equations,c onsidering the complexity of the diffuse r flow field,the flow can be treated as two dimensional due to large ratio of wi dth to high of the diffuser.From the com parison of calculation results with expe rimental data we find that the non linea r k ε model is better than the standard k ε model in predicting of pressure reco very and velocity distribution whether t here is flow separation or not in the fl ow field.The non linear k ε model can pr edict local separation at critical diver gent angle.As the rate of non linear dis tortion is included in the non linear k ε model which describes non homogeneous of turbulent fluctuating parameters,the non linear k ε model is suitable to more complicated flow field.The turbulent in tensity and the turbulent energy distrib ution in an asymmetrical diffuser are al so given by using two k ε models.
出处
《航空动力学报》
EI
CAS
CSCD
北大核心
1995年第1期59-62,共4页
Journal of Aerospace Power