Investigation of the relationship between the 3D flow structure and surface heat transfer within a realistic gas turbine blade trailing edge internal serpentine cooling channel
Author:
Funder
Korea Electric Power Corporation
Publisher
Elsevier BV
Subject
Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics
Reference39 articles.
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2. Experimental and numerical investigation of the flow in a trailing edge ribbed internal cooling passage;Baek;J. Turbomach.,2019
3. The effect of single-sided ribs on heat transfer and pressure drop within a trailing edge internal channel of a gas turbine blade;Kim;J. Therm. Sci. Eng. Appl.,2022
4. Heat transfer in a rib turbulated pin fin array for trailing edge cooling;Otto;J. Therm. Sci. Eng. Appl.,2022
5. Detailed studies on the flow field and heat transfer characteristics inside a realistic serpentine cooling channel with a S-shaped inlet;Funazaki,2018
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