共 50 条
- [32] Cooling of Turbine Blade Surface with Extended Exit Holes: Parametric Study ASME INTERNATIONAL MECHANICAL ENGINEERING CONGRESS AND EXPOSITION, 2014, VOL 6A, 2015,
- [33] NUMERICAL STUDY OF FILM COOLING ENHANCEMENT IN GAS TURBINE COMBUSTOR LINER IMECE 2008: HEAT TRANSFER, FLUID FLOWS, AND THERMAL SYSTEMS, VOL 10, PTS A-C, 2009, : 1237 - 1247
- [35] Cooling of Turbine Blades With Expanded Exit Holes: Computational Analyses of Leading Edge and Pressure-Side of a Turbine Blade JOURNAL OF ENERGY RESOURCES TECHNOLOGY-TRANSACTIONS OF THE ASME, 2017, 139 (04):