Micro cooling of a Gas Turbine Blade with a Shell-Spar Design
<p> The cooling effectiveness with the skin cooled micro cooling of a single gas turbine blade is analyzed numerically. The study use Hypermesh to generate a comprehensive 3D mesh of the domain that consists of air around the blade, skin layer of the blade, the cooling channels that wrap arou...
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| Language: | EN |
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Southern Illinois University at Edwardsville
2019
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| Online Access: | http://pqdtopen.proquest.com/#viewpdf?dispub=10975690 |