FEEDBACK CONTROL OF COMBUSTION OSCILLATIONS
By Ann P. Dowling, A. Morgans. 2005
301 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Computational Mechanics, Fluid Flow and Transfer Processes
View Paper: https://www.semanticscholar.org/paper/c47dcc7bf64464d5991d885ce157c0920aa35e99
How researchers see this paper
The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.
In Aerospace Engineering
In Computational Mechanics
In Fluid Flow and Transfer Processes
- A. Morgans
- Thierry Poinsot
- T. Schuller
- S. Candel
- R. Balachandran
- Jadeed Beita
- M. Talibi
- S. Sadasivuni
Citations in the corpus
- Thermoacoustic Instability Considerations for High Hydrogen Combustion in Lean Premixed Gas Turbine Combustors: A Review (2021, methodology): “Over time, the oscillations can result in substantial system deterioration while constraining the operating envelope of the engine [38] and in worst-case scenarios, lead to structural damage [39,40].”
- Tuned Passive Control of Combustion Instabilities Using Multiple Helmholtz Resonators (2007, background): “Typically, combustion instabilities are attenuated using either active or passive control by breaking the coupling between unsteady heat release and acoustic waves [2, 3].”
- Dynamics and control of premixed combustion systems based on flame transfer and describing functions (2020, background): “…combustion oscillations can be gauged in the successive reviews from Crocco & Cheng (1956); Putnam (1971); McManus et al. (1993); Candel (2002); Dowling & Morgans (2005); Lieuwen & Yang (2005); Culick (2006); Huang & Yang (2009); Gicquel et al. (2012); O’Connor et al. (2015); Poinsot (2017);…”