Impact of trailing-edge modification in stator vanes on heat ... - ATSLA
Seal slots are formed by an assembly of jaws. By changing jaw units, various seal designs can be easily tested. Motion of the jaws allows various offsets ...
SMALL GAS TURBINE ENGINE COMPONENT TECHNOLOGY - DTICIn both the cas- cade tests and the complete stage tests, measured temperatures of the stator spars and ancillary hot-section hardware verified the efficacy of. Loss Mechanisms in Turbomachines - UnifeConsidering 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.
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