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Bhavi RS, Sudarsanan S, Raghunathan M, Bhaskaran A, Sujith RI. Canard explosions in turbulent thermo-fluid systems. CHAOS (WOODBURY, N.Y.) 2024; 34:103133. [PMID: 39432718 DOI: 10.1063/5.0223320] [Citation(s) in RCA: 0] [Impact Index Per Article: 0] [Reference Citation Analysis] [Abstract] [Track Full Text] [Subscribe] [Scholar Register] [Received: 06/13/2024] [Accepted: 09/29/2024] [Indexed: 10/23/2024]
Abstract
A sudden transition to a state of high-amplitude periodic oscillations is catastrophic in a thermo-fluid system. Conventionally, upon varying the control parameter, a sudden transition is observed as an abrupt jump in the amplitude of the fluctuations in these systems. In contrast, we present an experimental discovery of a canard explosion in a turbulent reactive flow system where we observe a continuous bifurcation with a rapid rise in the amplitude of the fluctuations within a narrow range of control parameters. The observed transition is facilitated via a state of bursting, consisting of the epochs of large amplitude periodic oscillations amidst the epochs of low-amplitude periodic oscillations. The amplitude of the bursts is higher than the amplitude of the bursts of an intermittency state in a conventional gradual transition, as reported in turbulent reactive flow systems. During the bursting state, we observe that temperature fluctuations of the exhaust gas vary at a slower time scale in correlation with the amplitude envelope of the bursts. We also present a phenomenological model for thermoacoustic systems to describe the observed canard explosion. Using the model, we explain that the large amplitude bursts occur due to the slow-fast dynamics at the bifurcation regime of the canard explosion.
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Affiliation(s)
- Ramesh S Bhavi
- Department of Aerospace Engineering, Indian Institute of Technology Madras, Chennai, Tamil Nadu 600036, India
- Centre of Excellence for Studying Critical Transition in Complex Systems, Indian Institute of Technology Madras, Chennai, Tamil Nadu 600036, India
| | - Sivakumar Sudarsanan
- Department of Aerospace Engineering, Indian Institute of Technology Madras, Chennai, Tamil Nadu 600036, India
- Centre of Excellence for Studying Critical Transition in Complex Systems, Indian Institute of Technology Madras, Chennai, Tamil Nadu 600036, India
| | - Manikandan Raghunathan
- Department of Aerospace Engineering, Indian Institute of Technology Madras, Chennai, Tamil Nadu 600036, India
- Centre of Excellence for Studying Critical Transition in Complex Systems, Indian Institute of Technology Madras, Chennai, Tamil Nadu 600036, India
| | - Anaswara Bhaskaran
- Department of Aerospace Engineering, Indian Institute of Technology Madras, Chennai, Tamil Nadu 600036, India
- Centre of Excellence for Studying Critical Transition in Complex Systems, Indian Institute of Technology Madras, Chennai, Tamil Nadu 600036, India
| | - R I Sujith
- Department of Aerospace Engineering, Indian Institute of Technology Madras, Chennai, Tamil Nadu 600036, India
- Centre of Excellence for Studying Critical Transition in Complex Systems, Indian Institute of Technology Madras, Chennai, Tamil Nadu 600036, India
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Banerjee A, Pavithran I, Sujith RI. Early warnings of tipping in a non-autonomous turbulent reactive flow system: Efficacy, reliability, and warning times. CHAOS (WOODBURY, N.Y.) 2024; 34:013113. [PMID: 38198675 DOI: 10.1063/5.0160918] [Citation(s) in RCA: 0] [Impact Index Per Article: 0] [Reference Citation Analysis] [Abstract] [Track Full Text] [Subscribe] [Scholar Register] [Received: 06/06/2023] [Accepted: 12/04/2023] [Indexed: 01/12/2024]
Abstract
Real-world complex systems such as the earth's climate, ecosystems, stock markets, and combustion engines are prone to dynamical transitions from one state to another, with catastrophic consequences. State variables of such systems often exhibit aperiodic fluctuations, either chaotic or stochastic in nature. Often, the parameters describing a system vary with time, showing time dependency. Constrained by these effects, it becomes difficult to be warned of an impending critical transition, as such effects contaminate the precursory signals of the transition. Therefore, a need for efficient and reliable early-warning signals (EWSs) in such complex systems is in pressing demand. Motivated by this fact, in the present work, we analyze various EWSs in the context of a non-autonomous turbulent thermoacoustic system. In particular, we investigate the efficacy of different EWS in forecasting the onset of thermoacoustic instability (TAI) and their reliability with respect to the rate of change of the control parameter. This is the first experimental study of tipping points in a non-autonomous turbulent thermoacoustic system. We consider the Reynolds number (Re) as the control parameter, which is varied linearly with time at finite rates. The considered EWSs are derived from critical slowing down, spectral properties, and fractal characteristics of the system variables. The state of TAI is associated with large amplitude acoustic pressure oscillations that could lead thermoacoustic systems to break down. We consider acoustic pressure fluctuations as a potential system variable to perform the analysis. Our analysis shows that irrespective of the rate of variation of the control parameter, the Hurst exponent and variance of autocorrelation coefficients warn of an impending transition well in advance and are more reliable than other EWS measures. Additionally, we show the variation in the warning time to an impending TAI with rates of change of the control parameter. We also investigate the variation in amplitudes of the most significant modes of acoustic pressure oscillations with the Hurst exponent. Such variations lead to scaling laws that could be significant in prediction and devising control actions to mitigate TAI.
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Affiliation(s)
- Ankan Banerjee
- Department of Aerospace Engineering, Indian Institute of Technology Madras, Chennai 600036, India
- Center of Excellence for Studying Critical Transitions in Complex Systems, Indian Institute of Technology Madras, Chennai 600036, India
| | - Induja Pavithran
- Department of Aerospace Engineering, Indian Institute of Technology Madras, Chennai 600036, India
- Center of Excellence for Studying Critical Transitions in Complex Systems, Indian Institute of Technology Madras, Chennai 600036, India
| | - R I Sujith
- Department of Aerospace Engineering, Indian Institute of Technology Madras, Chennai 600036, India
- Center of Excellence for Studying Critical Transitions in Complex Systems, Indian Institute of Technology Madras, Chennai 600036, India
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Manoj K, Pawar SA, Kurths J, Sujith RI. Rijke tube: A nonlinear oscillator. CHAOS (WOODBURY, N.Y.) 2022; 32:072101. [PMID: 35907738 DOI: 10.1063/5.0091826] [Citation(s) in RCA: 0] [Impact Index Per Article: 0] [Reference Citation Analysis] [Abstract] [Track Full Text] [Subscribe] [Scholar Register] [Received: 03/17/2022] [Accepted: 06/16/2022] [Indexed: 06/15/2023]
Abstract
Dynamical systems theory has emerged as an interdisciplinary area of research to characterize the complex dynamical transitions in real-world systems. Various nonlinear dynamical phenomena and bifurcations have been discovered over the decades using different reduced-order models of oscillators. Different measures and methodologies have been developed theoretically to detect, control, or suppress the nonlinear oscillations. However, obtaining such phenomena experimentally is often challenging, time-consuming, and risky mainly due to the limited control of certain parameters during experiments. With this review, we aim to introduce a paradigmatic and easily configurable Rijke tube oscillator to the dynamical systems community. The Rijke tube is commonly used by the combustion community as a prototype to investigate the detrimental phenomena of thermoacoustic instability. Recent investigations in such Rijke tubes have utilized various methodologies from dynamical systems theory to better understand the occurrence of thermoacoustic oscillations and their prediction and mitigation, both experimentally and theoretically. The existence of various dynamical behaviors has been reported in single and coupled Rijke tube oscillators. These behaviors include bifurcations, routes to chaos, noise-induced transitions, synchronization, and suppression of oscillations. Various early warning measures have been established to predict thermoacoustic instabilities. Therefore, this review article consolidates the usefulness of a Rijke tube oscillator in terms of experimentally discovering and modeling different nonlinear phenomena observed in physics, thus transcending the boundaries between the physics and the engineering communities.
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Affiliation(s)
- Krishna Manoj
- Department of Mechanical Engineering, Massachusetts Institute of Technology, Cambridge, Massachusetts 02139, USA
| | - Samadhan A Pawar
- Department of Aerospace Engineering, Indian Institute of Technology Madras, Chennai 600036, India
| | - Jürgen Kurths
- Potsdam Institute for Climate Impact Research, Potsdam 14473, Germany
| | - R I Sujith
- Department of Aerospace Engineering, Indian Institute of Technology Madras, Chennai 600036, India
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Srikanth S, Pawar SA, Manoj K, Sujith RI. Dynamical states and bifurcations in coupled thermoacoustic oscillators. CHAOS (WOODBURY, N.Y.) 2022; 32:073129. [PMID: 35907737 DOI: 10.1063/5.0085273] [Citation(s) in RCA: 4] [Impact Index Per Article: 2.0] [Reference Citation Analysis] [Abstract] [Track Full Text] [Subscribe] [Scholar Register] [Received: 01/14/2022] [Accepted: 07/05/2022] [Indexed: 06/15/2023]
Abstract
The emergence of rich dynamical phenomena in coupled self-sustained oscillators, primarily synchronization and amplitude death, has attracted considerable interest in several fields of science and engineering. Here, we present a comprehensive theoretical study on the manifestation of these exquisite phenomena in a reduced-order model of two coupled Rijke tube oscillators, which are prototypical thermoacoustic oscillators. We characterize the dynamical behaviors of two such identical and non-identical oscillators by varying both system parameters (such as the uncoupled amplitudes and the natural frequencies of the oscillators) and coupling parameters (such as the coupling strength and the coupling delay). The present model captures all the dynamical phenomena-namely, synchronization, phase-flip bifurcation, amplitude death, and partial amplitude death-observed previously in experiments on coupled Rijke tubes. By performing numerical simulations and deriving approximate analytical solutions, we systematically decipher the conditions and the bifurcations underlying the aforementioned phenomena. The insights provided by this study can be used to understand the interactions between multiple cans in gas turbine combustors and develop control strategies to avert undesirable thermoacoustic oscillations in them.
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Affiliation(s)
- Sneha Srikanth
- Department of Mechanical Engineering, Indian Institute of Technology Madras, Chennai 600036, India
| | - Samadhan A Pawar
- Department of Aerospace Engineering, Indian Institute of Technology Madras, Chennai 600036, India
| | - Krishna Manoj
- Department of Mechanical Engineering, Massachusetts Institute of Technology, Cambridge, Massachusetts 02139, USA
| | - R I Sujith
- Department of Aerospace Engineering, Indian Institute of Technology Madras, Chennai 600036, India
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George NB, Raghunathan M, Unni VR, Sujith RI, Kurths J, Surovyatkina E. Preventing a global transition to thermoacoustic instability by targeting local dynamics. Sci Rep 2022; 12:9305. [PMID: 35661119 PMCID: PMC9166721 DOI: 10.1038/s41598-022-12951-6] [Citation(s) in RCA: 0] [Impact Index Per Article: 0] [Reference Citation Analysis] [Abstract] [Track Full Text] [Download PDF] [Figures] [Journal Information] [Subscribe] [Scholar Register] [Received: 03/25/2022] [Accepted: 05/16/2022] [Indexed: 11/09/2022] Open
Abstract
The burning of fossil fuels to generate power produces harmful emissions. Lowering such emissions in gas turbine engines is possible by operating them at fuel-lean conditions. However, such strategies often fail because, under fuel-lean conditions, the combustors are prone to catastrophic high-amplitude oscillations known as thermoacoustic instability. We reveal that, as an operating parameter is varied in time, the transition to thermoacoustic instability is initiated at specific spatial regions before it is observed in larger regions of the combustor. We use two indicators to discover such inceptive regions: the growth of variance of fluctuations in spatially resolved heat release rate and its spatiotemporal evolution. In this study, we report experimental evidence of suppression of the global transition to thermoacoustic instability through targeted modification of local dynamics at the inceptive regions. We strategically arrange slots on the flame anchor, which, in turn, reduce the local heat release rate fluctuations at the inceptive regions and thus suppress the global transition to thermoacoustic instability. Our results open new perspectives for combustors that are more environmental-friendly.
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Affiliation(s)
- Nitin Babu George
- Potsdam Institute for Climate Impact Research, Potsdam, Germany. .,Department of Physics, Humboldt University of Berlin, Berlin, Germany.
| | | | - Vishnu R Unni
- Department of Mechanical and Aerospace Engineering, Indian Institute of Technology, Hyderabad, India
| | - R I Sujith
- Department of Aerospace Engineering, Indian Institute of Technology, Madras, India
| | - Jürgen Kurths
- Potsdam Institute for Climate Impact Research, Potsdam, Germany.,Department of Physics, Humboldt University of Berlin, Berlin, Germany
| | - Elena Surovyatkina
- Potsdam Institute for Climate Impact Research, Potsdam, Germany.,Space Research Institute of Russian Academy of Sciences, Moscow, Russia
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Lee M, Guan Y, Gupta V, Li LKB. Input-output system identification of a thermoacoustic oscillator near a Hopf bifurcation using only fixed-point data. Phys Rev E 2020; 101:013102. [PMID: 32069669 DOI: 10.1103/physreve.101.013102] [Citation(s) in RCA: 12] [Impact Index Per Article: 3.0] [Reference Citation Analysis] [Abstract] [Track Full Text] [Journal Information] [Subscribe] [Scholar Register] [Received: 10/05/2019] [Indexed: 11/07/2022]
Abstract
We present a framework for performing input-output system identification near a Hopf bifurcation using data from only the fixed-point branch, prior to the Hopf point itself. The framework models the system with a van der Pol-type equation perturbed by additive noise, and identifies the system parameters via the corresponding Fokker-Planck equation. We demonstrate the framework on a prototypical thermoacoustic oscillator (a flame-driven Rijke tube) undergoing a supercritical Hopf bifurcation. We find that the framework can accurately predict the properties of the Hopf bifurcation and the limit cycle beyond it. This study constitutes an experimental demonstration of system identification on a reacting flow using only prebifurcation data, opening up pathways to the development of early warning indicators for nonlinear dynamical systems near a Hopf bifurcation.
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Affiliation(s)
- Minwoo Lee
- Department of Mechanical and Aerospace Engineering, The Hong Kong University of Science and Technology, Clear Water Bay, Hong Kong
| | - Yu Guan
- Department of Mechanical and Aerospace Engineering, The Hong Kong University of Science and Technology, Clear Water Bay, Hong Kong
| | - Vikrant Gupta
- Department of Mechanics and Aerospace Engineering, Southern University of Science and Technology, Shenzhen, China
| | - Larry K B Li
- Department of Mechanical and Aerospace Engineering, The Hong Kong University of Science and Technology, Clear Water Bay, Hong Kong
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Kasthuri P, Unni VR, Sujith RI. Bursting and mixed mode oscillations during the transition to limit cycle oscillations in a matrix burner. CHAOS (WOODBURY, N.Y.) 2019; 29:043117. [PMID: 31042964 DOI: 10.1063/1.5095401] [Citation(s) in RCA: 0] [Impact Index Per Article: 0] [Reference Citation Analysis] [Abstract] [Track Full Text] [Subscribe] [Scholar Register] [Received: 03/08/2019] [Accepted: 03/18/2019] [Indexed: 06/09/2023]
Abstract
We investigate the route to self-excited thermoacoustic instability in a laminar flow multiple flame matrix burner. With an increase in the equivalence ratio, the thermoacoustic system that is initially quiet (stable operation) transitions to limit cycle oscillations through two distinct dynamical states, namely, bursting oscillations and mixed mode oscillations. The acoustic pressure oscillations transition from quiescence to large amplitudes during bursting oscillations. Such high amplitude bursting oscillations that occur well ahead of the onset of limit cycle oscillations can potentially cause structural damage. The thermoacoustic system exhibits hysteresis. The transition to limit cycle oscillations is replicated in a phenomenological model containing slow-fast time scales.
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Affiliation(s)
- Praveen Kasthuri
- Department of Aerospace Engineering, Indian Institute of Technology Madras, Chennai 600036, India
| | - Vishnu R Unni
- Department of Mechanical and Aerospace Engineering, University of California San Diego, 9500 Gilman Dr., La Jolla, California 92093, USA
| | - R I Sujith
- Department of Aerospace Engineering, Indian Institute of Technology Madras, Chennai 600036, India
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Unni VR, Gopalakrishnan EA, Syamkumar KS, Sujith RI, Surovyatkina E, Kurths J. Interplay between random fluctuations and rate dependent phenomena at slow passage to limit-cycle oscillations in a bistable thermoacoustic system. CHAOS (WOODBURY, N.Y.) 2019; 29:031102. [PMID: 30927835 DOI: 10.1063/1.5088943] [Citation(s) in RCA: 5] [Impact Index Per Article: 1.0] [Reference Citation Analysis] [Abstract] [Track Full Text] [Subscribe] [Scholar Register] [Received: 01/10/2019] [Accepted: 03/11/2019] [Indexed: 06/09/2023]
Abstract
We study the impact of noise on the rate dependent transitions in a noisy bistable oscillator using a thermoacoustic system as an example. As the parameter-the heater power-is increased in a quasi-steady manner, beyond a critical value, the thermoacoustic system undergoes a subcritical Hopf bifurcation and exhibits periodic oscillations. We observe that the transition to this oscillatory state is often delayed when the control parameter is varied as a function of time. However, the presence of inherent noise in the system introduces high variability in the characteristics of this critical transition. As a result, if the value of the system variable-the acoustic pressure-approaches the noise floor before the system crosses the unstable manifold, the effect of rate on the critical transition becomes irrelevant in determining the transition characteristics, and the system undergoes a noise-induced tipping to limit-cycle oscillations. The presence of noise-induced tipping makes it difficult to identify the stability regimes in such systems by using stability maps for the corresponding deterministic system.
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Affiliation(s)
- Vishnu R Unni
- Department of Mechanical and Aerospace Engineering, University of California San Diego, San Diego, California 92093, USA
| | - E A Gopalakrishnan
- Center for Computational Engineering and Networking, Amrita School of Engineering, Coimbatore 641112, India
| | - K S Syamkumar
- Indian Institute of Technology Madras, Chennai 600036, India
| | - R I Sujith
- Indian Institute of Technology Madras, Chennai 600036, India
| | | | - Jürgen Kurths
- Potsdam Institute for Climate Impact Research, Berlin 14412, Germany
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