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- [1] Heat transfer experiment on film cooling of turbine blade leading edge Tan, Xiao-Ming, 1600, Beijing University of Aeronautics and Astronautics (BUAA) (29):
- [3] Experimental Investigation of Adiabatic Film Cooling Effectiveness and Heat Transfer Coefficients Over a Gas Turbine Blade Leading Edge Configuration INTERNATIONAL CONFERENCE ON MATERIAL SCIENCE AND MATERIAL ENGINEERING (MSME 2014), 2014, : 492 - 499
- [4] Effect of Film Cooling Arrangement on Impingement Heat Transfer on Turbine Blade Leading Edge PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2013, VOL 3A, 2013,
- [5] Convective heat transfer through film cooling holes of a gas turbine blade leading edge Proceedings of the ASME Turbo Expo 2005, Vol 3 Pts A and B, 2005, : 833 - 844
- [6] Experiment on Flow and Heat Transfer of Impingement-Film Cooling for Leading Edge of Turbine Blade Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics, 2020, 41 (12): : 2970 - 2976
- [7] HEAT TRANSFER BOUNDARY CONDITION WAVEFORMS ON A TURBINE BLADE LEADING EDGE WITH UNSTEADY FILM COOLING PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2013, VOL 3B, 2013,
- [8] Experimental investigation of leading edge film cooling heat transfer with a row of film cooling holes Tuijin Jishu/Journal of Propulsion Technology, 2008, 29 (03): : 290 - 294
- [9] Heat transfer enhancement in combined cooling of the turbine blade leading edge Russian Aeronautics, 2013, 56 (04): : 384 - 389
- [10] EXPERIMENTAL AND NUMERICAL INVESTIGATION OF EFFECT OF BLOWING RATIO ON FILM COOLING EFFECTIVENESS AND HEAT TRANSFER COEFFICIENT OVER A GAS TURBINE BLADE LEADING EDGE FILM COOLING CONFIGURATIONS PROCEEDINGS OF THE ASME GAS TURBINE INDIA CONFERENCE, 2013, 2014,