NOX reduction in an axially staged gas turbine model combustor through increase in the combustor exit Mach number

出版年份 2019 全文链接

标题

作者

关键词

出版物

Volume 212, Issue -, Pages 282-294

出版商

Elsevier BV

发表日期

2019-11-16

DOI

10.1016/j.combustflame.2019.10.039

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