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Numerical study of the effect of inlet geometry on combustion instabilities in a lean premixed swirl combustor
Numerical study of the effect of inlet geometry on combustion instabilities in a lean premixed swirl combustor
Numerical study of the effect of inlet geometry on combustion instabilities in a lean premixed swirl combustor
Lee, C. E. (Autor:in) / Park, S. H. (Autor:in) / Hwang, C. H. (Autor:in)
JOURNAL OF MECHANICAL SCIENCE AND TECHNOLOGY ; 30 ; 5293-5303
01.01.2016
11 pages
Aufsatz (Zeitschrift)
Englisch
DDC:
621
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Combustion Dynamics in a Model Lean-Premixed Gas Turbine with a Swirl Stabilized Injector
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