Heat transfer and film-cooling for the endwall of a first stage turbine vane
Author:
Publisher
Elsevier BV
Subject
Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics
Reference32 articles.
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4. Predictions of endwall losses and secondary flows in axial flow turbine cascades;Sharma;J. Turbomachinery,1987
5. Turbulent transport on the endwall in the region between adjacent turbine blades;Goldstein;ASME J. Heat Transfer,1988
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1. Experimental investigation on cooling performance and heat transfer characteristics of the ribbed endwall with upstream leakage;International Communications in Heat and Mass Transfer;2024-09
2. Effect of non-axisymmetric endwall contouring and swirling inlet flow on film cooling performance of turbine endwall;International Journal of Heat and Mass Transfer;2024-09
3. A comparative study of purge slot exit shape on the film cooling effectiveness of a gas turbine shroud;International Journal of Thermal Sciences;2024-03
4. Numerical investigation on film cooling and aerodynamic performance for gas turbine endwalls with upstream vane-type and cascade-type slots;Aerospace Science and Technology;2024-02
5. Heat Transfer and Film Cooling in an Aggressive Turbine Center Frame;Journal of Turbomachinery;2023-10-19
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