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- [3] Film cooling with compound angle holes in leading edge of twisted turbine blade Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2023, 44 (18):
- [6] Analysis on film cooling hole arrangement effect for rotating blade leading edge Hangkong Dongli Xuebao/Journal of Aerospace Power, 2023, 38 (06): : 1340 - 1349
- [7] ROTATING FILM COOLING PERFORMANCE OF THE HOLE NEAR THE LEADING EDGE ON THE SUCTION SIDE OF THE TURBINE BLADE PROCEEDINGS OF THE ASME INTERNATIONAL MECHANICAL ENGINEERING CONGRESS AND EXPOSITION, 2018, VOL 8B, 2019,
- [8] Numerical simulation of film cooling in leading edge of turbine blade Hangkong Dongli Xuebao, 2009, 3 (519-525): : 519 - 525
- [9] Enhancement of film cooling performance at the leading edge of turbine blade PROCEEDINGS OF THE ASME TURBO EXPO 2006, VOL 3, PTS A AND B: HEAT TRANSFER: GENERAL INTEREST, 2006, : 307 - 313