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Experiment study of aerodynamic performance for the . . . Abstract The influences of suction-side and pressure-side winglet-cavity tips on the flow field and aerodynamic performance of a turbine blade with tip clearance have been investigated in a low-speed cascade wind tunnel
Effects of Turbine Blade Tip Pressure Side Winglet and Cavity Rim on . . . In this study, numerical analysis showed that a large fraction of the leakage flow occurs after 50% of the axial chord Thus, an additional rim was installed at the mid-point of the cavity, in an attempt to block the leakage flow to the suction side and redirect it back to the pressure side
Experimental and numerical investigations for turbine aerodynamic . . . In this research, wind tunnel experiments and numerical calculations are performed for the Original Cavity Tip (OCT), the modified Stepped Cavity Tip (SCT) and Cavity Winglet Tip (CWT) with different pressure squealers under seven incidence angles in a range of ±15°
Sci-Hub | Experiment study of aerodynamic performance for the suction . . . Experimental Thermal and Fluid Science, 90, 220–230 | 10 1016 j expthermflusci 2017 09 020 Zhou, Z , Chen, S , Li, W , Wang, S , Zhou, X (2018) Experiment study of aerodynamic performance for the suction-side and pressure-side winglet-cavity tips in a turbine blade cascade