燃气轮机过渡段双腔室模型设计及优化
刘光洁1,2, 徐涛1, 李俊楼1, 于征磊3, 修航1, 程飞1

Design and optimization of double chamber model of gas turbine transition piece
LIU Guang-jie1,2, XU Tao1, LI Jun-lou1, YU Zheng-lei3, XIU Hang1, CHENG Fei1
图3 冲击孔及风向倾角示意图
Fig.3 Diagram of the impinging hole' angle and injection orientation