Effects of rotating blade wakes on separation and pressure recovery in turbine exhaust diffusers

Proceedings of the ASME Turbo Expo

Volumn 6, Issue PART C, 2008, Pages 1921-1931

  Sieker, Olaf ^a   Seume, Joerg R ^a  

^a LEIBNIZ UNIVERSITY HANNOVER   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AXIAL VELOCITY; BLADED ROTORS; CONICAL DIFFUSER; DESIGN POINTS; DESIGN VALUE; FLOW COEFFICIENTS; GAS TURBINE EXHAUSTS; HIGH ENERGY; INLET SWIRLS; LASER DOPPLER; LOW SWIRL; MASS FLOW; NUMERICAL DESIGN; OPENING ANGLE; OPERATING POINTS; PNEUMATIC PROBE; PRESSURE RECOVERY; ROTATING BLADES; SCALE MODELS; STATIC PRESSURE; SWIRL NUMBERS; TURBINE EXHAUST; TURBINE ROTOR; TURBULENT CHARACTERISTICS; TURBULENT WAKE; UNSTEADY INTERACTION; VARIABLE SPEED; VELOCITY PROFILES;

ATMOSPHERIC THERMODYNAMICS; BOUNDARY LAYERS; ELECTRIC DRIVES; ENGINES; FLOW PATTERNS; GAS TURBINES; RECOVERY; ROTATION; SEPARATION; WAKES; WHEELS;

ELECTRIC GENERATORS;

EID: 69949124454     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2008-50788     Document Type: Conference Paper

References (13)

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