Effect of colored noise on precursors of thermoacoustic instability in model gas turbine combustors

被引:0
作者
Vishnoi, Neha [1 ]
Gupta, Vikrant [2 ]
Saurabh, Aditya [3 ]
Kabiraj, Lipika [1 ]
机构
[1] Indian Inst Technol Ropar, Rupnagar, Punjab, India
[2] Southern Univ Sci & Technol, Shenzhen, Guangdong, Peoples R China
[3] Indian Inst Technol Kanpur, Kanpur, Uttar Pradesh, India
关键词
Coherence resonance; Colored noise; Gas turbine combustors; Hopf bifurcation; Hurst exponent; Precursors; Thermoacoustic instability; Van der Pol oscillator; COHERENCE RESONANCE; DRIVEN; BIFURCATIONS; OSCILLATIONS; DYNAMICS;
D O I
10.1177/17568277241262168
中图分类号
O414.1 [热力学];
学科分类号
摘要
In this work, we numerically investigate the dynamics of a prototypical thermoacoustic system, the generalized Van der Pol oscillator, in the presence of additive noise of varying color (correlation time) and intensity while the system undergoes supercritical and subcritical Hopf bifurcation. We specifically investigate the influence of noise color on trends in the coherence factor and the Hurst exponent in the subthreshold region to assess their reliability as instability precursors. The Hurst exponent is found reliable only for correlation times much larger than the time scale of the instability while the coherence factor is found to be reliable for the entire range of noise color investigated. These inferences are found to hold for both supercritical and subcritical bifurcation cases.
引用
收藏
页码:80 / 92
页数:13
相关论文
共 27 条
  • [21] Experimental study on impacts of fuel type on thermo-acoustic instability in a gas turbine model combustor
    Ruan, Can
    Chen, FeiEr
    Yu, Tao
    Cai, WeiWei
    He, ZhuoYao
    Mao, YeBing
    Li, XinLing
    Lu, XingCai
    SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2021, 64 (06) : 1345 - 1358
  • [22] Effect of CO2 Opposing Multiple Jets on Thermoacoustic Instability and NOx Emissions in a Lean-Premixed Model Combustor
    Hao Zhou
    Liubin Hu
    Journal of Thermal Science, 2024, 33 : 207 - 221
  • [23] Effect of CO2 Opposing Multiple Jets on Thermoacoustic Instability and NOx Emissions in a Lean-Premixed Model Combustor
    Zhou, Hao
    Hu, Liubin
    JOURNAL OF THERMAL SCIENCE, 2024, 33 (01) : 207 - 221
  • [24] The Effect of Partial Premixing and Heat Loss on the Reacting Flow Field Prediction of a Swirl Stabilized Gas Turbine Model Combustor
    Goevert, Simon
    Mira, Daniel
    Kok, Jim B. W.
    Vazquez, Mariano
    Houzeaux, Guillaume
    FLOW TURBULENCE AND COMBUSTION, 2018, 100 (02) : 503 - 534
  • [25] Effect of fuel-feeding excitation on the isothermal turbulent swirling flow structure in a lean gas turbine model combustor
    Hashim, Mohamed Y.
    Bae, Jonggeun
    Dafsari, Reza Alidoost
    Lee, Jeekeun
    INTERNATIONAL COMMUNICATIONS IN HEAT AND MASS TRANSFER, 2023, 148
  • [26] THE EFFECT OF TRANSIENT FUEL STAGING ON SELF-EXCITED INSTABILITIES IN A MULTI-NOZZLE MODEL GAS TURBINE COMBUSTOR
    Culler, Wyatt
    Samarasinghe, Janith
    Quay, Bryan D.
    Santavicca, Domenic A.
    O'Connor, Jacqueline
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2017, VOL 4A, 2017,
  • [27] Investigation into the cause of high multi-mode combustion instability of H2/CO/CH4 syngas in a partially premixed gas turbine model combustor
    Lee, Min Chul
    Yoon, Jisu
    Joo, Seongpil
    Kim, Jeongjin
    Hwang, Jeongjae
    Yoon, Youngbin
    PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2015, 35 : 3263 - 3271