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dc.contributor.authorRedjem, Aymen
dc.contributor.authorYahiaoui, Imad Eddine; Ranane, Rachid (promoteur); Chegrani, Ahmed (promoteur)
dc.date.accessioned2021-05-05T07:39:01Z
dc.date.available2021-05-05T07:39:01Z
dc.date.issued2020
dc.identifier.urihttp://di.univ-blida.dz:8080/jspui/handle/123456789/11392
dc.descriptionMémoire de Master.-Numéro de Thèse126/2020fr_FR
dc.description.abstractThis work is a contribution to the numerical study of gas turbine cycles, more specifically; it studies the final state of combustion. The numerical analysis is based on a ten-dissociation sub-reactions kinetic model of Ethylene, which allows the calculation of the reaction products molar fractions using a Newton-Raphson method based Matlab code, which at first requires the calculation of the Jacobian matrix for the 11 variables system. The mole numbers will be then injected into a Bisection method based Matlab code, which uses the both, the reactants and products enthalpy to guess the adiabatic flame temperature up to a maximum precision. The study also includes an Ansys simulation of a combustor model made in SolidWorks with the measures of the P9005 micro-gas turbine combustor, which allows for a comparison between the Matlab Program Results, the simulation results and some results and benchmarks runs from different articles. The study also includes the effect of pre-heat inlet air on the final temperature and the parameters contributing to the production of pollutant in the products.fr_FR
dc.language.isoenfr_FR
dc.publisherUniversité Blida 01fr_FR
dc.titleNumerical sydy of the reactive flow behaviour in gas turbine combustorfr_FR
dc.typeThesisfr_FR
Collection(s) :Mémoires de Master

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