Numerical study of the effect of inlet geometry on combustion instabilities in a lean premixed swirl combustor
Author:
Publisher
Springer Science and Business Media LLC
Subject
Mechanical Engineering,Mechanics of Materials
Link
http://link.springer.com/content/pdf/10.1007/s12206-016-1048-y.pdf
Reference37 articles.
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4. T. Lieuwen, H. Torres, C. Johnson and B. T. Zinn, A mechanism of combustion instability in lean premixed gas turbine combustor, The American Society of Mechanical Engineers, ASME paper 99-GT-3 (1999).
5. K. C. Schadow, E. Gutmark, T. P. Parr, D. M. Parr, K. J. Wilson and J. E. Crump, Large-scale coherent structures as drivers of combustion instability, Combustion Science and Technology, 64 (4-6) (1989) 167–186.
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