Heat transfer and pressure distributions on a gas turbine blade tip

Journal of Turbomachinery

Volumn 122, Issue 4, 2000, Pages 717-724

  Azad, Gm S ^a   Han, J C ^a   Teng, S ^a   Boyle, R J ^a  

^a Texas AandM University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BLADE; GAS TURBINE; HEAT TRANSFER; PRESSURE DISTRIBUTION;

EID: 0034531624     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1308567     Document Type: Conference Paper

References (18)

1. The effect of relative motion, blade edge radius and gap size on the blade tip pressure distribution in an annular turbine cascade with clearance
2. The measurement and formation of tip clearance loss
3. Flow and heat transfer in turbine tip gaps
4. Effects of simulated rotation on tip leakage in a planar cascade of turbine blades: Part I-Tip gap flow
5. Measurements of the flow in an idealized turbine tip gap
6. The effect of tip clearance on the development of loss behind a rotor and a subsequent nozzle
7. Heat transfer at the tip of an unshrouded turbine blade
8. Cavity heat transfer on a transverse grooved wall in a narrow flow channel
9. Heat transfer in the tip region of grooved turbine blades
10. Heat transfer and flow for a grooved turbine blade tip in a transonic cascade
11. Turbine tip and shroud heat transfer
12. Heat transfer and flow on the first stage blade tip of a power generation gas turbine: Part I-Experimental results
13. Prediction of unshrouded rotor blade tip heat transfer
14. Analysis of gas turbine rotor blade tip and shroud heat transfer
15. Effect of squealer tip on rotor heat transfer and efficiency
16. Effects of tip clearance and casing recess on heat transfer and stage efficiency in axial turbines
17. Heat transfer and flow on the first stage blade tip of a power generation gas turbine: Part 2-Simulation results
18. Describing uncertainties in single sample experiments