An experimental study of surface temperature distribution on effusion-cooled plates

Journal of Engineering for Gas Turbines and Power

Volumn 123, Issue 2, 2001, Pages 308-316

  Bernhard Gustafsson, K M ^a   Gunnar Johansson, T ^a  

^a CHALMERS UNIVERSITY OF TECHNOLOGY   (Sweden)

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTION CHAMBERS; TEMPERATURE DISTRIBUTION; THERMAL CONDUCTIVITY; THERMOGRAPHY (IMAGING);

EFFUSION-COOLED PLATES;

GAS TURBINES;

COOLING; HEAT TRANSFER; PLATE; TEMPERATURE DISTRIBUTION;

EID: 0035302993     PISSN: 07424795     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1364496     Document Type: Article

References (14)

1. Heat (Mass) transfer and film cooling effectiveness with injection through discrete holes: Part i-within holes and on the back surface
2. Heat (Mass) transfer and film cooling effectiveness with injection through discrete holes: Part ii- On the exposed surface
3. The flow and film cooling effectiveness following injection through a row of holes
4. Distribution of film-cooling effectiveness on a turbine endwall measured using the Ammonia and Diazo technique
5. Adiabatic wall effectiveness measurements of film-cooling holes with expanded exits
6. Detailed measurements of local heat transfer coefficient and adiabatic wall temperature beneath and array of impinging jets
7. An experimental study of film cooling effectiveness near the leading edge of a turbine blade
8. Film cooling from Spanwise-oriented holes in two staggered rows
9. Analysis of film cooling and full coverage film cooling of gas turbine blades
10. Heat and mass transfer problems for film cooling
11. Full-coverage discrete hole film cooling: Investigation of the effect of variable density ratio
12. Row-of-hole film cooling of curved walls at low injection angles