Heat transfer and flow on the blade tip of a gas turbine equipped with a mean-camberline strip

Journal of Turbomachinery

Volumn 123, Issue 4, 2001, Pages 704-708

  Ameri, A A ^a  

^a AYT Corporation   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATION THEORY; HEAT TRANSFER; HEAT TRANSFER COEFFICIENTS; TURBOMACHINE BLADES;

MEAN-CAMBERLINE STRIPS;

GAS TURBINES;

BLADE; GAS TURBINE; HEAT TRANSFER; MATHEMATICAL ANALYSIS;

EID: 0035483102     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1400114     Document Type: Article

References (14)

1. Heat transfer at the tip of an unshrouded turbine blade
2. Heat transfer and flow on the first-stage blade tip of a power generation gas turbine: Part 2-simulation results
3. Heat Transfer and Flow on the First-Stage Blade Tip of a Power generation gas turbine: Part I-Experimental results
4. An experimental study of heat transfer and flow on a gas turbine blade tip with various tip leakage sealing methods
5. Effect of squealer tip on rotor heat transfer and efficiency
6. Development of an explicit multiblock/multigrid flow solver for viscous flows in complex geometries
7. Multigrid calculation of three dimensional viscous cascade flows
8. Internal passage heat transfer prediction using multiblock grids and k-w turbulence model
9. Numerical prediction of heat transfer in a channel with ribs and bleed
10. Simulation of transition with a two-equation turbulence model
11. Zonal two-equation k-w turbulence models for aerodynamic flows
12. Effects of tip clearance and casing recess on heat transfer and stage efficiency in axial turbines