2019
DOI: 10.1007/s11071-019-04815-y
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Bifurcation dodge: avoidance of a thermoacoustic instability under transient operation

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Cited by 29 publications
(4 citation statements)
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“…To investigate the transition from S C to S TI via S IN , we perform experiments on a laboratory scale turbulent combustor (Komarek and Polifke 2010, Unni et al 2015, Silva et al 2017 and acquire spatiotemporal data. Our study analyses the transition between the dynamical states by continuously varying a system parameter, the air mass flow rate ( ṁair ) from low to high values (Gopalakrishnan et al 2016, Bonciolini and Noiray 2019, Pavithran and Sujith 2021. In all the experiments, we increase ṁair from 537 ± 8 SLPM to 780 ± 10 SLPM linearly with time.…”
Section: Analysis Of Fluctuations In the Global Observablesmentioning
confidence: 99%
“…To investigate the transition from S C to S TI via S IN , we perform experiments on a laboratory scale turbulent combustor (Komarek and Polifke 2010, Unni et al 2015, Silva et al 2017 and acquire spatiotemporal data. Our study analyses the transition between the dynamical states by continuously varying a system parameter, the air mass flow rate ( ṁair ) from low to high values (Gopalakrishnan et al 2016, Bonciolini and Noiray 2019, Pavithran and Sujith 2021. In all the experiments, we increase ṁair from 537 ± 8 SLPM to 780 ± 10 SLPM linearly with time.…”
Section: Analysis Of Fluctuations In the Global Observablesmentioning
confidence: 99%
“…Bonciolini et al [154] investigated the ratedependent transition delay along with the effect of noise in a laboratory-scale combustor system. In a quent study, Bonciolini and Noiray [155] presented a method of bifurcation dodging to avoid thermoacoustic instability by varying the parameter at fast rates. In a recent experimental study, Manikandan and Sujith [156] reported R-tipping to thermoacoustic instability via intermittency in a turbulent afterburner.…”
Section: Continuous Variation Of Control Parametersmentioning
confidence: 99%
“…To investigate the transition from S C to S TI via S IN , we perform experiments on a laboratory scale turbulent combustor 39,[55][56][57][58] and acquire spatiotemporal data. Our study analyses the transition between the dynamical states by continuously varying a system parameter, the air mass flow rate (ṁ air ) from low to high values 47,[59][60][61][62] . In all the experiments, we increaseṁ air from 537 ±8 SLPM (SLPM denotes standard liters per minute) to 780 ±10 SLPM linearly with time.…”
Section: Analysis Of Fluctuations In the Global Observablesmentioning
confidence: 99%