Exploring liquid fuel combustion dynamics in a swirl burner using dynamic mode decomposition
Aero gas turbine engine combustors are transitioning from traditional Rich-Quench-Lean (RQL) staging to Lean Premixed Prevaporized (LPP) operation to reduce harmful NOx emissions and improve combustion efficiency.
Alireza Ghasemi, Jim B. W. Kok
doaj +1 more source
Time Series and Spectral Analysis of Thermoacoustic Oscillations for Propane-Oxyfuel Combustion in a Swirl-Stabilized, Nonpremixed Combustor. [PDF]
Talal Q +4 more
europepmc +1 more source
In this study, the effects of various system parameters on combustion instability were numerically identified through a network-based thermoacoustic model using the concept of a transfer function.
Seonyeong Kim, Daesik Kim
doaj +1 more source
Modeling and control of thermoacoustic instabilities
This work deals with modeling and control of thermoacoustic combustion instabilities in lean premixed combustion systems. Because of the complex interactions present in thermoacoustic systems, a network modeling approach is used. The model of each network element or subsystem is obtained analytically, numerically, or by making use of experimental ...
openaire +1 more source
Analysis of Combustion Instability of Methane-Air Premixed Swirling Flame Based on OH-PLIF Measurements. [PDF]
Deng K, Xue C, Liu Z, Hu J, Zhong Y.
europepmc +1 more source
Thermoacoustic instability remains an important challenge in gas turbines. In can-annular combustors, cross-talk effects can lead to complex collective dynamics.
Yichen Wang +7 more
doaj +1 more source
Steady-state statistics, emergent patterns and intermittent energy transfer in a ring of oscillators. [PDF]
Pedergnana T, Noiray N.
europepmc +1 more source
All-optical light-induced thermoacoustic spectroscopy for remote and non-contact gas sensing. [PDF]
Pan Y +9 more
europepmc +1 more source
Review of acoustic field effects on flame dynamics and combustion applications
Acoustic-flame coupling technology is an interdisciplinary frontier field investigating the complex interactions between sound waves and combustion. Generally, the acoustic field can be divided into two modes based on its relative position to the flame ...
Zhiwei Su, Yaoyao Ying, Dong Liu
doaj +1 more source
Study on thermoacoustic instabilities in an aircraft engine combustor using 1D network model
The purpose of this study was to evaluate the combustion instability characteristics of target aircraft combustors under development using network thermoacoustic (TA) models.
Juchan Son +3 more
doaj +1 more source

