The role of rotor tip clearance on the aerodynamic interaction of a last gas turbine stage and an exhaust diffuser

Proceedings of the ASME Turbo Expo

Volumn 1, Issue , 1998, Pages

  Willinger, Reinhard ^a   Haselbacher, Hermann ^a  

^a VIENNA UNIVERSITY OF TECHNOLOGY   (Austria)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRCRAFT ENGINES; FLOW FIELDS; FLOW OF FLUIDS; GASES; TURBINE COMPONENTS; TURBOMACHINE BLADES; WIND TUNNELS;

AERODYNAMIC INTERACTIONS; CASCADE WIND TUNNELS; END-WALL REGION; GAS TURBINE STAGES; INTERACTION MODEL; NUMERICAL INVESTIGATIONS; PRESSURE RECOVERY; ROTOR TIP CLEARANCE;

GAS TURBINES;

EID: 84867761698     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/98-GT-094     Document Type: Conference Paper

References (18)

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