SMALL GAS TURBINE ENGINE COMPONENT TECHNOLOGY - DTIC
In 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. VARIABLE STATOR RADIAL TURBINETesting 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.
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