TY - GEN
T1 - Prediction of thermoacoustic instabilities in a premixed combustor based on FFT-based dynamic characterization
AU - Mondal, Sudeepta
AU - Bhattacharya, Chandrachur
AU - Chattopadhyay, Pritthi
AU - Mukhopadhyay, Achintya
AU - Ray, Asok
PY - 2017/1/1
Y1 - 2017/1/1
N2 - The classification of a combustion process into stable and unstable regimes is essential for the design of combustor systems, which include their monitoring and control mechanisms; an unsupervised method for monitoring of combustion instabilities is essential from these perspectives. The traditional methods of combustion stability assessment are often computationally intensive and thus may not be suitable for real-time monitoring and control. This paper proposes a fast Fourier transform (FFT)-based method for dynamic characterization of combustion instabilities. The proposed method has been tested on experimental data of pressure time-series from a lean-premixed swirl-stabilized combustor, and the results have been compared with the well-known method of visibility graph.
AB - The classification of a combustion process into stable and unstable regimes is essential for the design of combustor systems, which include their monitoring and control mechanisms; an unsupervised method for monitoring of combustion instabilities is essential from these perspectives. The traditional methods of combustion stability assessment are often computationally intensive and thus may not be suitable for real-time monitoring and control. This paper proposes a fast Fourier transform (FFT)-based method for dynamic characterization of combustion instabilities. The proposed method has been tested on experimental data of pressure time-series from a lean-premixed swirl-stabilized combustor, and the results have been compared with the well-known method of visibility graph.
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M3 - Conference contribution
SN - 9781624105111
T3 - 53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017
BT - 53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017
Y2 - 10 July 2017 through 12 July 2017
ER -