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Feedback control of combustion instabilities from within limit cycle oscillations using [Formula: see text] loop-shaping and the ν-gap metric

Combustion instabilities arise owing to a two-way coupling between acoustic waves and unsteady heat release. Oscillation amplitudes successively grow, until nonlinear effects cause saturation into limit cycle oscillations. Feedback control, in which an actuator modifies some combustor input in respo...

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Detalles Bibliográficos
Autores principales: Li, Jingxuan, Morgans, Aimee S.
Formato: Online Artículo Texto
Lenguaje:English
Publicado: The Royal Society Publishing 2016
Materias:
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC4971234/
https://www.ncbi.nlm.nih.gov/pubmed/27493558
http://dx.doi.org/10.1098/rspa.2015.0821