Please use this identifier to cite or link to this item: https://hdl.handle.net/20.500.11851/5800
Title: Investigation of the effect of co/counter configurations of a double swirler airblast atomizer in an annular turbojet combustor with computational fluid dynamics
Authors: Bolat, Hasan Başar
Uslu, S.
Issue Date: 2015
Publisher: American Institute of Aeronautics and Astronautics Inc, AIAA
Source: 51st AIAA/SAE/ASEE Joint Propulsion Conference, 2015, 27 July 2015 through 29 July 2015, , 130539
Abstract: Strong mixing of fuel and air is one of the most important parameter ín combustion design criteria. Air-blast atomizer has two important functions in combustion chamber. One of them is to atomize the liquid fuel, and the second one is to enable good mixing of the fuel and air in the flametube by creating a swirling and re-circulating flow in the primary zone. This strong mixing can be achieved by swirler channels of the air-blast atomizers. In this study, the effects of the co- and counter-swirl configurations of a double swirler airblast atomizer on flow field, temperature distribution and exit emissions in an annular turbojet combustor is investigated by CFD. ANSYS-Fluent software is used for CFD simulations. Flamelet combustion model was used for modelling of the non-premixed combustion. Simulation results of temperature distribution, equivalence ratio and NOx emissions are presented and discussed. © 2015, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
URI: https://doi.org/10.2514/6.2015-3787
https://hdl.handle.net/20.500.11851/5800
ISBN: 9781624103216
Appears in Collections:Makine Mühendisliği Bölümü / Department of Mechanical Engineering
Scopus İndeksli Yayınlar Koleksiyonu / Scopus Indexed Publications Collection

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