共 50 条
- [11] Heat mass transfer analog of air-cooling rotating dise with naphthalene sublimation Journal of Aerospace Power/Hangkong Dongli Xuebao, 1993, 8 (03):
- [13] Heat Transfer Coefficient and Film Cooling Effectiveness on the Partial Cavity Tip of a Gas Turbine Blade JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2019, 141 (07):
- [14] HEAT TRANSFER COEFFICIENT AND FILM COOLING EFFECTIVENESS ON THE PARTIAL CAVITY TIP OF A GAS TURBINE BLADE PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, 2018, VOL 5C, 2018, : 379 - 388
- [15] MEASUREMENT OF DETAILED HEAT TRANSFER COEFFICIENT AND FILM COOLING EFFECTIVENESS DISTRIBUTIONS USING PSP AND TSP PROCEEDINGS OF THE ASME TURBO EXPO 2009, VOL 3, PTS A AND B, 2009, : 807 - 817
- [16] The variation of heat transfer coefficient, adiabatic effectiveness and aerodynamic loss with film cooling hole shape HEAT TRANSFER IN GAS TURBINE SYSTEMS, 2001, 934 : 361 - 368
- [17] Film cooling effectiveness and mass heat transfer coefficient downstream of one row of discrete holes JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1999, 121 (02): : 225 - 232
- [18] Film cooling effectiveness and mass/heat transfer coefficient downstream of one row of discrete holes Journal of Turbomachinery, 1999, 121 (02): : 225 - 232
- [19] EXPERIMENTAL STUDY ON LOCAL HEAT TRANSFER IN A ROTATING, TWO-PASS COOLING CHANNEL WITH DENSE ARRAY OF TURBULENCE PROMOTERS WITH NAPHTHALENE SUBLIMATION METHOD PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2014, VOL 5A, 2014,
- [20] 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,