Loss Mechanisms in Turbomachines - Unife

Considering first shrouded blades, the flow over the shrouded turbine blade with a single tip seal is illustrated in Fig. 29. The leaking flow contracts to ...







Influence of cavity flow on turbine aerodynamics - isae supaero
... stator interaction provided additional phenomena compared to the linear cas ... Blade losses . . . . . . . . . . . . . . . . . . . . . . . . . . . . 59.
VARIABLE STATOR RADIAL TURBINE
Testing was conducted at design rated speed and pressure ratio over a range of flow from 62 to 120 percent of design. Overall performance and rotor exit survey.
THÈSE
Cet air sert à alimenter les cavités en pied de turbine sous la plateforme pour refroidir les disques rotor.



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SMALL GAS TURBINE ENGINE COMPONENT TECHNOLOGY - DTIC