共 50 条
- [42] Numerical investigation on aerodynamic loss of turbine cascade with converging slot hole film cooling at suction surface Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2010, 31 (07): : 1312 - 1317
- [43] EXPERIMENTAL INVESTIGATION OF SWEEPING JET FILM COOLING IN A TRANSONIC TURBINE CASCADE PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, 2019, VOL 5B, 2019,
- [44] Process and analysis of cooling structure design for gas turbine rotor blades with film cooling Zhongguo Dianji Gongcheng Xuebao/Proceedings of the Chinese Society of Electrical Engineering, 2015, 35 (16): : 4112 - 4121
- [45] THE INFLUENCE OF BOUNDARY LAYER STATE AND TRAILING EDGE WEDGE ANGLE ON THE AERODYNAMIC PERFORMANCE OF TRANSONIC TURBINE BLADES PROCEEDINGS OF ASME TURBO EXPO 2022: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2022, VOL 10B, 2022,
- [46] New Supersonic Loss Model for the Preliminary Design of Transonic Turbine Blades and the Influence of Pitch JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2020, 142 (04):
- [47] The Influence of Boundary Layer State and Trailing Edge Wedge Angle on the Aerodynamic Performance of Transonic Turbine Blades JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2023, 145 (04):
- [48] Aerodynamic performance of a family of three high pressure transonic turbine blades at off-design incidence Proceedings of the ASME Turbo Expo 2005, Vol 6, Pts A and B, 2005, : 451 - 464
- [49] EFFECT OF FILM COOLING HOLES SHAPE OF HELIUM TURBINE BLADES IN HTGR PROCEEDINGS OF THE 24TH INTERNATIONAL CONFERENCE ON NUCLEAR ENGINEERING, 2016, VOL 3, 2016,