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- [4] 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):
- [6] THE MEASUREMENT OF BOUNDARY-LAYERS ON A COMPRESSOR BLADE IN CASCADE .2. SUCTION SURFACE BOUNDARY-LAYERS JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1988, 110 (01): : 138 - 145
- [9] NUMERICAL STUDY OF BLADE TIP COOLING AT HIGH SPEED WITH TIP AND PRESSURE-SIDE COOLANT INJECTIONS PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, 2018, VOL 5A, 2018,