Aerothermal efficiency of a ribbed channel in an internal gas turbine blade cooling system

Proceedings of the 7th European Conference on Turbomachinery: Fluid Dynamics and Thermodynamics, ETC 2007

Volumn , Issue , 2007, Pages

  Shevchuk, I V ^a   Jenkins, S ^a   Von Wolfersdorf, J ^a   Weigand, B ^a  

^a UNIVERSITY OF STUTTGART   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; FLOW OF FLUIDS; GAS TURBINES; HEAT TRANSFER; LIQUID CRYSTALS; NUMERICAL MODELS; THERMOELECTRIC EQUIPMENT; TURBINE COMPONENTS; TURBOMACHINE BLADES; TURBULENCE MODELS;

AEROTHERMAL; BLADE COOLING SYSTEMS; CHANNEL HEIGHT; FLUID FLOW AND HEAT TRANSFERS; GAS TURBINE BLADE COOLING; GAS TURBINE BLADES; INDUSTRIAL GAS TURBINES; INTERNAL COOLING; RIBBED CHANNELS; WIDTH RATIO;

COOLING SYSTEMS;

EID: 85185136341     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (17)

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