轴流压气机考虑展向掺混的数值计算  

Numerical Calculation of Axial Compressor Considering Spanwise Mixing

作　　者：李涛[1] 吴亚东[1,2] 欧阳华[1,3] LI Tao;WU Ya-dong;OUYANG Hua(School of Mechanical Engineering, Shanghai Jiao Tong University, Shanghai 200240, China;Institute of Gas Turbine, Shanghai Jiao Tong University, Shanghai 200240, China;Collaborative Innovation Center for Advanced Aero-Engine, Beijing 100083, China)

机构地区：[1]上海交通大学机械与动力工程学院,上海200240 [2]上海交通大学燃气轮机研究院,上海200240 [3]上海交通大学先进航空发动机协同创新中心,北京100083

出　　处：《航空发动机》2018年第2期87-91,共5页Aeroengine

摘　　要：为了更加准确地反映压气机内部流场的展向分布特性并提高计算精度,基于流线曲率法发展了1种考虑压气机内部展向掺混作用的计算方法。应用Gallimore-Cumpst y(G-C)掺混模型模拟紊流扩散的作用,在2维Cart er公式基础上引入改善的Rober t s修正模型对落后角进行预估,通过落后角反映二次流的作用,并对3级轴流压气机3S1进行了计算分析和比较。结果表明:不考虑掺混因素时所得计算数据的展向分布情况与实际流场相差较大;只有同时考虑紊流掺混和二次流2种因素,才能得到最优结果。该方法能够较好地模拟轴流压气机的展向掺混作用,得到更加贴近实际的气动参数分布,可为压气机设计和优化提供参考。In order to reflect the spanwise distribution characteristics of inner flow field of compressor more accurately and to improve calculation accuracy,a calculation method considering spanwise mixing in the axial compressor was developed,based on streamline curvature method.The turbulent diffusion was simulated by applying Gallimore-Cumpsty（G-C）mixing model.The deviation angle,which was used to reflect the effect of secondary flow,was predicted by the modified Roberts model based on the Carter＇s 2 D formula.and the computational analysis and comparison of a three-stage axial compressor 3 S1 were performed.The results show that the spanwise distribution of the calculation taking no account of mixing is much different from the actual flow field,and the optimal results can be achieved only if turbulent diffusion and secondary flow are considered simultaneously.The method can simulate the spanwise mixing performance of axial compressors better and obtain reliable aerodynamic parameter distribution,which is helpful to the design and optimization of compressor.

关 键 词：气动设计 轴流压气机 流线曲率法 展向掺混 落后角 

分 类 号：V231.3[航空宇航科学与技术—航空宇航推进理论与工程]