共 50 条
- [21] Cooling and heat transfer characteristics of high-pressure turbine blade with cutback squealer tip Hangkong Dongli Xuebao/Journal of Aerospace Power, 2019, 34 (10): : 2131 - 2139
- [22] MEASUREMENT OF BLADE TIP HEAT TRANSFER AND LEAKAGE FLOW IN A TURBINE CASCADE WITH A MULTI-CAVITY SQUEALER TIP PROCEEDINGS OF THE ASME TURBINE BLADE TIP TECHNICAL SYMPOSIUM, 2013, 2014,
- [24] Effect of squealer geometry arrangement on a gas turbine blade tip heat transfer JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME, 2002, 124 (03): : 452 - 459
- [25] Heat transfer coefficients on the squealer tip and near-tip regions of a gas turbine blade with single or double squealer JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2003, 125 (04): : 778 - 787
- [27] CHARACTERISTICS OF TIP LEAKAGE FLOW OF THE TURBINE BLADE WITH CUTBACK SQUEALER AND COOLANT INJECTION PROCEEDINGS OF THE ASME TURBO EXPO 2010: TURBOMACHINERY: AXIAL FLOW FAN AND COMPRESSOR AERODYNAMICS DESIGN METHODS, AND CFD MODELING FOR TURBOMACHINERY, VOL 7, PTS A-C, 2010, : 1243 - 1251
- [29] Effects of Oval-Hole and Inclination Angle on the Flow and Heat Transfer Performance of the Turbine Blade with Squealer Tip Wang, Xinjun, 1600, Xi'an Jiaotong University (55): : 153 - 161
- [30] Heat transfer coefficients and film cooling effectiveness on the squealer tip of a gas turbine blade JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2003, 125 (04): : 648 - 657