R Zhu, D Pan, C Ji, T Zhu, P Lu, H Gao - Energy, 2020 - Elsevier
The combustion instability of a partially premixed swirl burner is investigated by experimental tests and numerical modeling. The experimental results show that the …
R Sampath, SR Chakravarthy - Combustion and Flame, 2016 - Elsevier
The present work deals with time-resolved investigation of the flow field during acoustic self- excitation by a lean premixed flame in a dump combustor. Simultaneous measurements of …
S Ha, T Lieuwen - Combustion and Flame, 2025 - Elsevier
There are several mechanisms through which turbulent flames produce sound. In low Mach number, unconfined flows, direct combustion noise–ie, unsteady gas expansion generated …
Y Wang, CH Sohn, J Bae, Y Yoon - Aerospace Science and Technology, 2021 - Elsevier
The flame transfer function (FTF) and acoustic transfer function (ATF) are estimated experimentally and numerically, respectively, and both are combined to predict combustion …
M Yoon - Journal of Sound and Vibration, 2020 - Elsevier
This paper presents a one-dimensional thermoacoustic model for a dump combustor in terms of two acoustic impedances just before and after a flame/area-expansion location. A …
M Yoon - Journal of Sound and Vibration, 2022 - Elsevier
This paper presents a thermoacoustic model in the frequency domain for multi-burner combustors composed of multiple plenum-nozzle-chamber modules with cross-talk at both …
AM Kypraiou, PM Allison, A Giusti… - Combustion Science …, 2018 - Taylor & Francis
The response of three flames with different degrees of premixedness (fully premixed, non- premixed with radial, and non-premixed with axial fuel injection) to acoustic oscillations is …
J Kim, M Yoon, D Kim - Journal of the Korean Society of …, 2016 - koreascience.kr
In this paper we propose a new approach for an analysis and a prediction of combustion instability of lean premixed gas turbines. Our approach is based on the Nyquist stability …
MG Yoon, D Kim - Journal of Mechanical Science and Technology, 2017 - Springer
In this study we develop an analytic thermoacoustic model of a combustor for gas turbines. The combustor under consideration is composed of a premixing chamber, a nozzle, and a …