Effects of Rotor Tip Blade Loading Variation on Compressor Stage Performance
نویسندگان
چکیده
منابع مشابه
Assessment of various rotor tip geometries on a single stage gas turbine performance
Tip leakage loss introduces major part of losses of the rotor in axial gas turbines. Therefore, the rotor blade tip has a considerable effect on rotor efficiency. To understand the flow physics of the rotor tip leakage, we solve the flow field for different tip platforms (passive flow control) and by considering coolant tip injection (active flow control). Various blade tip configurations s...
متن کاملassessment of various rotor tip geometries on a single stage gas turbine performance
tip leakage loss introduces major part of losses of the rotor in axial gas turbines. therefore, the rotor blade tip has a considerable effect on rotor efficiency. to understand the flow physics of the rotor tip leakage, we solve the flow field for different tip platforms (passive flow control) and by considering coolant tip injection (active flow control). various blade tip configurations such ...
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15 صفحه اولEffects of Different Turbulence Models in Simulation of Unsteady Tip Leakage Flow in Axial Compressor Rotor Blades Row
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ژورنال
عنوان ژورنال: Journal of Turbomachinery
سال: 2017
ISSN: 0889-504X,1528-8900
DOI: 10.1115/1.4035252