1.By using nonoverlapping domain method,a 3-D viscous code had been developed to calculate flow field in a cascade with tip clearance and craping along casing.
本文给出基于区域分解算法的可考虑动叶顶和机匣刮削作用的涡轮计算方法。
2.Abstract: By using nonoverlapping domain method,a 3-D viscous code had been developed to calculate flow field in a cascade with tip clearance and craping along casing.