Extension of the Combustion Stability Range in Dry Low NOx Lean Premixed Gas Turbine Combustor Using a Fuel Rich Annular Pilot Burner (vol 136, 051509, 2014)

被引：0
|
作者：
Rosentsvit, L. [1 ]
机构：
[1] Technion Israel Inst Technol, Fac Aerosp Engn, IL-3200003 Haifa, Israel
来源：
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME | 2014年 / 136卷 / 08期
关键词：
D O I：
10.1115/1.4026906
中图分类号：
TH [机械、仪表工业];
学科分类号：
0802 ;
摘要：
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页数：1
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