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- [2] Film cooling downstream at a row of discrete holes with compound angle JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2001, 123 (02): : 222 - 230
- [3] SENSITIVITY ANALYSIS OF FLOW CONDITIONS AND GEOMETRIC PARAMETERS ON THE FILM COOLING EFFECTIVENESS FOR A FLAT TEST PLATE, PART 1: SINGLE ROW OF CYLINDRICAL HOLES FILM COOLING HT2009: PROCEEDINGS OF THE ASME SUMMER HEAT TRANSFER CONFERENCE 2009, VOL 2, 2009, : 529 - 538
- [5] Effect of forward expansion angle on film cooling characteristics of shaped holes OPEN PHYSICS, 2020, 18 (01): : 302 - 314
- [6] Cooling Performance of Single-Row Cylindrical Film Holes on Suction Side of a Rotor Blade Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics, 2021, 42 (03): : 595 - 600
- [8] PARAMETRIC COOLING STUDY OF SINGLE-ROW CYLINDRICAL FILM HOLES ON PRESSURE SIDE OF A ROTOR BLADE PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2017, VOL 5A, 2017,
- [9] Effect of rotation on film cooling with a single row of shaped holes on blade pressure side JOURNAL OF THERMAL SCIENCE AND TECHNOLOGY, 2017, 12 (02):
- [10] Influence of compound angle on adiabatic film cooling effectiveness and heat transfer coefficient for a row of shaped film cooling holes PROCEEDINGS OF THE ASME TURBO EXPO 2005, VOL 3 PTS A AND B, 2005, : 39 - 47