A two-dimensional, compressible flow model for loss created by the mixing behind the turbine cascade with coolant injection is presented, based on the theory developed by Denton.

• 基于Denton的尾缘流动理论 ,发展了一种考虑冷气喷射的二维、可压涡轮叶栅尾缘混合损失模型 ,研究了涡轮叶栅尾缘损失的特征 ,定量评估了影响尾缘损失的各种参数。