Affiliation of Author(s):能源与动力学院
Journal:INTERNATIONAL JOURNAL OF HYDROGEN ENERGY
Key Words:Gas turbine engine Lean direct injection Low emissions combustion
Abstract:Combustion characteristics in a hydrogen fuelled single-element lean direct injection (LDI) combustor for low emission gas turbine engine are computationally investigated. A single element LDI combustor was produced and simulated with steady-state Reynolds-averaged Navier Stokes reacting computations. Reacting computations of the single-element LDI combustor were performed with an augmented reduced 23-step reaction mechanism for hydrogen/air. A realizable k - epsilon model was used to obtain turbulence closure. For the single-element LDI combustor with different equivalence ratio, the effective area, axial velocity, total pressure drop coefficient, total temperature, mass fraction of OH, emission index of pollutant NO (EINO) were achieved and discussed. (C) 2016 Hydrogen Energy Publications LLC. Published by Elsevier Ltd. All rights reserved.
ISSN No.:0360-3199
Translation or Not:no
Date of Publication:2017-02-02
Co-author:Yuan, Li,Mongia, Hukam C.
Correspondence Author:Li Jianzhong
Professor
Supervisor of Doctorate Candidates
Alma Mater:南京航空航天大学
Education Level:南京航空航天大学
Degree:Doctoral Degree in Engineering
School/Department:能源与动力学院
Discipline:Thermal Engineering. Engineering Thermophysics. Aerospace Propulsion Theory and Engineering
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