The Aerodynamics of trailing-edge-cooled transonic turbine blades: Part 1 - Experimental approach

Proceedings of the ASME Turbo Expo

Volumn 1, Issue , 1997, Pages

  Deckers, Mathias ^a   Denton, John D ^b  

^a SIEMENS POWER GENERATION   (United States)

^b UNIVERSITY OF CAMBRIDGE   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; BOUNDARY LAYERS; COOLANTS; FIGHTER AIRCRAFT; FLOW OF FLUIDS; GAS TURBINES; PRESSURE EFFECTS; SUPERSONIC AIRCRAFT; TRANSONIC AERODYNAMICS; TURBOMACHINE BLADES;

COOLANT PRESSURE; EXPERIMENTAL APPROACHES; FLAT PLATE MODELS; SURFACE STATIC PRESSURE; TEMPERATURE RATIO; TRAILING EDGES; TRANSONIC TURBINE; TWO-DIMENSIONAL FLOW;

AERODYNAMICS;

EID: 84973652799     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/97-GT-518     Document Type: Conference Paper

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