Flow structures in a lean-premixed swirl-stabilized combustor with microjet air injection

@inproceedings{LaBry2011FlowSI,
  title={Flow structures in a lean-premixed swirl-stabilized combustor with microjet air injection},
  author={Z. LaBry and Santosh J. Shanbhogue and R. L. Speth and A. Ghoniem},
  year={2011}
}
Abstract The major challenge facing the development of low-emission combustors is combustion instability. By lowering flame temperatures, lean-premixed combustion has the potential to nearly eliminate emissions of thermally generated nitric oxides, but the chamber acoustics and heat release rate are highly susceptible to coupling in ways that lead to sustained, high-amplitude pressure oscillations, known as combustion instability. At different operating conditions, different modes of… Expand
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