Experimental investigation on cooling performance and heat transfer characteristics of the ribbed endwall with upstream leakage
Author:
Funder
National Major Science and Technology Projects of China
Publisher
Elsevier BV
Reference29 articles.
1. Turbine endwall cooling and heat transfer characteristics under slashface leakage interacted with nearby discrete-hole injections;Zhang;Int. J. Therm. Sci.,2021
2. Numerical analysis of vane endwall film cooling and heat transfer with different mainstream turbulence intensities and blowing ratios;Yang;Int. J. Therm. Sci.,2022
3. Study of effects of axisymmetric endwall contouring on film cooling/heat transfer and secondary losses in a cascade of first stage nozzle guide vane;Hussain;Appl. Therm. Eng.,2020
4. The effects of axisymmetric convergent contouring and blowing ratio on Endwall film cooling and vane pressure side surface phantom cooling performance;Bai;J. Eng. Gas Turbines Power,2021
5. Effects of varying non-axisymmetric contours of the turbine endwall on aerodynamics and heat transfer Aspects: a sensitivity analysis study;Chen;Int. J. Therm. Sci.,2021
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