We present an experimental study on the nonlinear dynamics of combustion instability in a lean premixed gas-turbine model combustor with a swirl-stabilized turbulent flame. Intermittent combustion oscillations switching irregularly back and forth between burst and pseudo-periodic oscillations exhibit the deterministic nature of chaos. This is clearly demonstrated by considering two nonlinear forecasting methods: an extended version (Gotoda et al., 2015, “Nonlinear Forecasting of the Generalized Kuramoto-Sivashinsky Equation,” Int. J. Bifurcation Chaos, 25, p. 1530015) of the Sugihara and May algorithm (Sugihara and May, 1990, “Nonlinear Forecasting as a Way of Distinguishing Chaos From Measurement Error in Time Series,” Nature, 344, pp. 734–741) as a local predictor, and a generalized radial basis function (GRBF) network as a global predictor (Gotoda et al., 2012, “Characterization of Complexities in Combustion Instability in a Lean Premixed Gas-Turbine Model Combustor,” Chaos, 22, p. 043128; Gotoda et al., 2016 (unpublished)). The former enables us to extract the short-term predictability and long-term unpredictability of chaos, while the latter can produce surrogate data to test for determinism by a free-running approach. The permutation entropy based on a symbolic sequence approach is estimated for the surrogate data to test for determinism and is also used as an online detector to prevent lean blowout.
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April 2017
Research-Article
Dynamical Properties of Combustion Instability in a Laboratory-Scale Gas-Turbine Model Combustor
Hiroshi Gotoda,
Hiroshi Gotoda
Department of Mechanical Engineering,
Tokyo University of Science,
6-3-1 Niijuku,
Katsushika, Tokyo 125-8585, Japan
e-mail: gotoda@rs.tus.ac.jp
Tokyo University of Science,
6-3-1 Niijuku,
Katsushika, Tokyo 125-8585, Japan
e-mail: gotoda@rs.tus.ac.jp
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Kenta Hayashi,
Kenta Hayashi
Department of Mechanical Engineering,
Ritsumeikan University,
1-1-1 Nojihigashi,
Kusatsu, Shiga 525-8577, Japan
Ritsumeikan University,
1-1-1 Nojihigashi,
Kusatsu, Shiga 525-8577, Japan
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Ryosuke Tsujimoto,
Ryosuke Tsujimoto
Department of Mechanical Engineering,
Ritsumeikan University,
1-1-1 Nojihigashi,
Kusatsu, Shiga 525-8577, Japan
Ritsumeikan University,
1-1-1 Nojihigashi,
Kusatsu, Shiga 525-8577, Japan
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Shohei Domen,
Shohei Domen
Department of Mechanical Engineering,
Ritsumeikan University,
1-1-1 Nojihigashi,
Kusatsu, Shiga 525-8577, Japan
Ritsumeikan University,
1-1-1 Nojihigashi,
Kusatsu, Shiga 525-8577, Japan
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Shigeru Tachibana
Shigeru Tachibana
Aeronautical Technology Directorate,
Japan Aerospace Exploration Agency,
7-44-1 Jindaiji-Higashi,
Chofu, Tokyo 182-8522, Japan
Japan Aerospace Exploration Agency,
7-44-1 Jindaiji-Higashi,
Chofu, Tokyo 182-8522, Japan
Search for other works by this author on:
Hiroshi Gotoda
Department of Mechanical Engineering,
Tokyo University of Science,
6-3-1 Niijuku,
Katsushika, Tokyo 125-8585, Japan
e-mail: gotoda@rs.tus.ac.jp
Tokyo University of Science,
6-3-1 Niijuku,
Katsushika, Tokyo 125-8585, Japan
e-mail: gotoda@rs.tus.ac.jp
Kenta Hayashi
Department of Mechanical Engineering,
Ritsumeikan University,
1-1-1 Nojihigashi,
Kusatsu, Shiga 525-8577, Japan
Ritsumeikan University,
1-1-1 Nojihigashi,
Kusatsu, Shiga 525-8577, Japan
Ryosuke Tsujimoto
Department of Mechanical Engineering,
Ritsumeikan University,
1-1-1 Nojihigashi,
Kusatsu, Shiga 525-8577, Japan
Ritsumeikan University,
1-1-1 Nojihigashi,
Kusatsu, Shiga 525-8577, Japan
Shohei Domen
Department of Mechanical Engineering,
Ritsumeikan University,
1-1-1 Nojihigashi,
Kusatsu, Shiga 525-8577, Japan
Ritsumeikan University,
1-1-1 Nojihigashi,
Kusatsu, Shiga 525-8577, Japan
Shigeru Tachibana
Aeronautical Technology Directorate,
Japan Aerospace Exploration Agency,
7-44-1 Jindaiji-Higashi,
Chofu, Tokyo 182-8522, Japan
Japan Aerospace Exploration Agency,
7-44-1 Jindaiji-Higashi,
Chofu, Tokyo 182-8522, Japan
Contributed by the Combustion and Fuels Committee of ASME for publication in the JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER. Manuscript received June 30, 2016; final manuscript received August 11, 2016; published online November 8, 2016. Editor: David Wisler.
J. Eng. Gas Turbines Power. Apr 2017, 139(4): 041509 (6 pages)
Published Online: November 8, 2016
Article history
Received:
June 30, 2016
Revised:
August 11, 2016
Citation
Gotoda, H., Hayashi, K., Tsujimoto, R., Domen, S., and Tachibana, S. (November 8, 2016). "Dynamical Properties of Combustion Instability in a Laboratory-Scale Gas-Turbine Model Combustor." ASME. J. Eng. Gas Turbines Power. April 2017; 139(4): 041509. https://doi.org/10.1115/1.4034700
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