旋转气冷涡轮三维流场的实验与数值研究  

Experimental Measurement and Numerical Simulation of Three-dimensional Flow Field in Rotating Film-cooled Turbine

作　　者：袁锋[1] 竺晓程[1] 杜朝辉[1] 

机构地区：[1]上海交通大学机械与动力工程学院,上海市徐汇区200030

出　　处：《中国电机工程学报》2008年第2期82-87,共6页Proceedings of the CSEE

基　　金：国家自然科学基金项目(50406017)。~~

摘　　要：采用k-ε湍流模型对气冷涡轮在静止和旋转2种工况下三维流场进行数值计算,并与PIV测量结果进行对比。计算得到射流和主流的掺混区域三维速度以及射流尾迹区二次流动,k-ε湍流模型的计算结果与实验基本吻合。与静止涡轮流场相比,旋转状态下涡轮内部流场中存在的离心力、哥氏力的作用使射流与主流掺混流场三维速度发生改变,其中径向速度的改变明显。计算和实验结果表明,旋转对气冷涡轮叶片压力面侧流场的影响大于吸力面。同时,吹风比增大使射流与主流掺混流场区域以及射流尾迹区的范围扩大。Numerical simulations of the three-dimensional flow field in the film-cooled turbine on the rotating and stationary conditions were carried out using k-ε turbulence model, and predictions of the three-dimensional velocity were compared with the particle image velocimeter （PIV） experimental measurements. Computational results reveal the mixing flow field of the jet and the mainstream and the secondary flow near the blade surface in the wake region, and the simulations are in fairly good agreement with the experiments. Compared with the stationary condition, there are centrifugal force and Coriolis force existing in the flow field of the turbine on the rotating condition, and these forces make the three-dimensional flow field changed in the rotating turbine, especially for the radial velocity. The effect of rotation on the flow field of the pressure side is more apparent than that of the suction side in the film-cooled turbine from the computational and measured results. The increase of the blowing ratio makes the mixing region and the wake region downstream of the injection hole expanded.

关 键 词：气膜冷却涡轮 旋转状态 静止状态 三维流场 激光粒子测速仪测量 数值计算 

分 类 号：V231[航空宇航科学与技术—航空宇航推进理论与工程]