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1 Geometry
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1 ResultSimulate the temperature distribution in turbine blades due to combustion gases and assess cooling efficiency through internal blade cooling channels. - Copy - Copy
1 Geometry 1 Mesh 1 Simulation setup 1 ResultSimulate the temperature distribution in turbine blades due to combustion gases and assess cooling efficiency through internal blade cooling channels. - Copy - Copy
by simscalesimscale
mmadriaga created this project
26 days ago
jetengine copied this project
25 days ago
