Simulation par fluent du refroidissement des aubes d'une turbine a gaz

Please use this identifier to cite or link to this item: http://archives.univ-biskra.dz/handle/123456789/2425

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DC Field	Value	Language
dc.contributor.author	M. Mansouri	-
dc.contributor.author	N. Belghar	-
dc.date.accessioned	2014-04-23T13:00:05Z	-
dc.date.available	2014-04-23T13:00:05Z	-
dc.date.issued	2014-04-23	-
dc.identifier.uri	http://archives.univ-biskra.dz/handle/123456789/2425	-
dc.description.abstract	This article concerns a study analytically and numerically the cooling of the dawn of a gas turbine. We used the Fluent software to simulate the aerodynamic effects and the thermal influence on the blade. We are interested primarily in the theoretical study of this technique applied to film cooling of a flat plate and then looking at the numerical simulation by Fluent model with a k-e turbulence standard was used to model the turbulent flow where there is much more interested in the thermal aspect of this type of flow trying to explore the effect of temperature on the blade. Link http://ijcps.net/index.php/IJCPS/article/view/5	en_US
dc.language.iso	en	en_US
dc.subject	gas turbine; convection; turbulence k-e; code Fluent.	en_US
dc.title	Simulation par fluent du refroidissement des aubes d'une turbine a gaz	en_US
dc.type	Article	en_US
Appears in Collections:	Publications Internationales

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