Z Rao, R Li, B Zhang, B Wang, D Zhao… - Aerospace Science and …, 2021 - Elsevier
In this work, the dynamics of the pressure oscillations and flame behaviors in a premixed swirl-stabilized combustor were experimentally investigated. As equivalence ratio Φ varied …
U Jin, KT Kim - Combustion and Flame, 2021 - Elsevier
Lean-premixed fuel-flexible combustion technology capable of operating on a wide range of fuels, including high or pure hydrogen, is expected to play a crucial role in reducing nitrogen …
F Chen, C Ruan, T Yu, W Cai, Y Mao, X Lu - Aerospace Science and …, 2019 - Elsevier
In this study, influences of fuel variation and inlet air temperature on the combustion stability characteristics in a gas turbine model combustor were experimentally investigated. Test …
Z Lyu, X Jia, Y Yang, K Hu, F Zhang, G Wang - Fuel, 2021 - Elsevier
In this paper, we propose a deep learning model to detect combustion instability using high- speed flame image sequences. The detection model combines Convolutional Neural …
U Jin, KT Kim - Combustion and Flame, 2022 - Elsevier
The utilization of hydrogen-blended hydrocarbon fuels, or even completely carbon-free fuels like pure hydrogen and ammonia, will be indispensable in the effort to reduce anthropogenic …
H Jegal, K Moon, J Gu, LKB Li, KT Kim - Combustion and Flame, 2019 - Elsevier
In a can-annular gas turbine combustion system, low-frequency self-excited combustion instabilities can arise from coupled interactions between adjacent can combustors, rather …
The influence of the injection system on combustion instabilities is investigated on a laboratory-scale combustor equipped with a single injector that is weakly-transparent to …
K Moon, H Jegal, C Yoon, KT Kim - Combustion and Flame, 2020 - Elsevier
The prediction of self-excited combustion instabilities in a can-annular gas turbine combustion system is a significant challenge, mainly because the instabilities originate from …
K Moon, H Jegal, J Gu, KT Kim - Combustion and Flame, 2019 - Elsevier
Longitudinal-mode combustion instabilities in can-annular gas turbine combustion systems are influenced by acoustic interactions between adjacent combustors; these interactions …