Journal
PHYSICAL REVIEW E
Volume 89, Issue 2, Pages -Publisher
AMER PHYSICAL SOC
DOI: 10.1103/PhysRevE.89.022910
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Funding
- Paloma Environmental Technology Foundation
- Adaptable & Seamless Technology Transfer Program through Target-Driven R&D from Japan Science and Technology Agency (JST)
- Ministry of Education, Culture, Sports, Science, and Technology of Japan (MEXT)
- Grants-in-Aid for Scientific Research [23686037] Funding Source: KAKEN
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We propose an online method of detecting combustion instability based on the concept of dynamical system theory, including the characterization of the dynamic behavior of combustion instability. As an important case study relevant to combustion instability encountered in fundamental and practical combustion systems, we deal with the combustion dynamics close to lean blowout (LBO) in a premixed gas-turbine model combustor. The relatively regular pressure fluctuations generated by thermoacoustic oscillations transit to low-dimensional intermittent chaos owing to the intermittent appearance of burst with decreasing equivalence ratio. The translation error, which is characterized by quantifying the degree of parallelism of trajectories in the phase space, can be used as a control variable to prevent LBO.
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