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- [5] CONJUGATE HEAT TRANSFER ANALYSIS FOR GAS TURBINE FILM-COOLED BLADE PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2016, VOL 5A, 2016,
- [6] HEAT TRANSFER COEFFICIENT AND ADIABATIC EFFECTIVENESS ON A FILM-COOLED PRESSURE SIDE: RESULTS AND ASSESSMENT OF THE IR-BASED MEASUREMENT TECHNIQUE RELIABILITY PROCEEDINGS OF ASME TURBO EXPO 2022: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2022, VOL 6A, 2022,
- [7] EFFECT OF ACCELERATION ON THE HEAT-TRANSFER COEFFICIENT ON A FILM-COOLED SURFACE JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1991, 113 (03): : 464 - 471
- [8] Film cooling effectiveness on the leading edge of a rotating film-cooled blade using pressure sensitive paint PROCEEDINGS OF THE ASME TURBO EXPO 2005, VOL 3 PTS A AND B, 2005, : 375 - 384
- [9] Heat Transfer Coefficient Measurements on the Film-Cooled Pressure Surface of a Transonic Airfoil JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2013, 135 (06):