Modeling the air-cooled gas turbine: Part 2-Coolant flows and losses

Journal of Turbomachinery

Volumn 124, Issue 2, 2002, Pages 214-221

  Young, J B ^a   Wilcock, R C ^a  

^a UNIVERSITY OF CAMBRIDGE   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

COOLANTS; COOLING; ENTROPY; THERMAL BARRIER COATINGS;

FLOWRATES;

GAS TURBINES;

AIR; COOLANT; COOLING; GAS TURBINE;

EID: 0036542009     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1415038     Document Type: Article

References (7)

1. Modelling the air-cooled gas turbine: Part I - General thermodynamics
2. Rotor blade cooling in high pressure turbines
3. Prediction of cooling flow requirements for advanced utility gas turbines: Part I: Analysis and scaling of the effectiveness curve; part II: Influence of ceramic thermal barrier coatings
4. On thermodynamics of gas turbine cycles: Part II - A model for expansion in cooled turbines
5. Effect of blade cooling system with minimized gas temperature dilution on gas turbine performance
6. Prediction of effects of mass-transfer cooling on the blade-row efficiency of turbine airfoils