ttncwt_CombSciTech20_accept.pdf (2.51 MB)
The effects of turbulence on jet stability and the flame transfer function in a lean-burn combustor
journal contribution
posted on 2020-07-29, 14:31 authored by Nick Treleaven, Andrew GarmoryAndrew Garmory, Gary PageGary PageLarge eddy simulations show that the penetration of the central jet in a multipassage lean burn and liquid fuelled combustor is dependent on the turbulence levels
in the three air-flow passages of the injector. These simulations are performed using
an incompressible method where an unsteady boundary condition is applied to the
inlets of a truncated domain which only includes the domain downstream of the
fuel injector using the recently developed Proper Orthogonal Decomposition Fourier
Series method. The fluctuating inlets are built from a combination of compressible
URANS data and incompressible LES data. This incompressible method is shown
to be consistent with fully compressible simulations whilst requiring only one third
of the computing time. Neglecting the turbulence generated in the passages results
in the incorrect penetration of the central jet, resulting in a flame transfer function
with a similar gain but with a different phase. Furthermore, large scale helical modes,
previously detected in non-reacting simulations of a similar burner geometry are seen
to be imprinted onto the liquid fuel spray, mixture fraction and heat release fields.
This shows that coupling between hydrodynamic instabilities and thermoacoustic
instabilities in liquid fuelled engines may be more significant than suggested by
previous studies of gas fuelled engines.
Funding
CDT in Gas Turbine Aerodynamics : EP/L015943/1
CFD Modelling of the acoustic response of sprays : Karen Muncey
History
School
- Aeronautical, Automotive, Chemical and Materials Engineering
Department
- Aeronautical and Automotive Engineering
Published in
Combustion Science and TechnologyVolume
192Issue
11Pages
2115 - 2137Publisher
Informa UK LimitedVersion
- AM (Accepted Manuscript)
Rights holder
© Taylor and FrancisPublisher statement
This is an Accepted Manuscript of an article published by Taylor & Francis in Combustion Science and Technology on 18 Jul 20, available online: https://doi.org/10.1080/00102202.2020.1777992Acceptance date
2020-06-01Publication date
2020-07-18Copyright date
2020ISSN
0010-2202eISSN
1563-521XPublisher version
Language
- en