Laboratory Investigations of Low-Swirl Injectors Operating With Syngases
Author:
Affiliation:
1. Environmental Energy Technology Division, Lawrence Berkeley National Laboratory, Berkeley, CA 94720
2. School of Aerospace Engineering, Georgia Institute of Technology, Atlanta, GA 30332
Abstract
Publisher
ASME International
Subject
Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering
Link
http://asmedigitalcollection.asme.org/gasturbinespower/article-pdf/doi/10.1115/1.3124662/5706912/011502_1.pdf
Reference20 articles.
1. A Comparison of the Flowfields and Emissions of High-Swirl Injectors and Low-Swirl Injectors for Lean Premixed Gas Turbines;Johnson;Proc. Combust. Inst.
2. Nazeer, W. A., Smith, K. O., Sheppard, P., Cheng, R. K., and Littlejohn, D., 2006, “Full Scale Testing of a Low Swirl Fuel Injector Concept for Ultra-Low NOx Gas Turbine Combustion Systems,” ASME Paper No. GT2006-90150.
3. Laboratory Study of Premixed H2-Air & H2–N2-Air Flames in a Low-Swirl Injector for Ultra-Low Emissions Gas Turbines;Cheng;ASME J. Eng. Gas Turbines Power
4. Laboratory Studies of the Flow Field Characteristics of Low-Swirl Injectors for Application to Fuel-Flexible Turbines;Cheng;ASME J. Eng. Gas Turbines Power
5. Fuel Effects on a Low-Swirl Injector for Lean Premixed Gas Turbines;Littlejohn;Proc. Combust. Inst.
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