Non-linear Flame Oscillations in a Multi-swirl Combustor
Author:
Affiliation:
1. University of Cincinnati College of Engineering and Applied Science
2. Indian Institute of Technology Kanpur
3. Indian Institute of Technology Ropar
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2022-2063
Reference30 articles.
1. Dolan, B. "Flame Interactions and Thermoacoustics in Multiple-Nozzle Combustors," Ph.D. Dissertation, Gas Dynamics and Propulsion lab, Department of Aerospace and Engineering Mechanics,University of Cincinnati, 2016
2. Kasthuri, P., Unni, V. and R., Sujith, R., I. "Bursting and Mixed Mode Oscillations during the transition to Limit Cycle Oscillations in a Matrix Burner", Chaos 29, 043117 (2019)
3. Experimental Investigation of Limit-Cycle Oscillations in an Unstable Gas Turbine Combustor
4. Recurrence plots for the analysis of complex systems
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