Experimental investigation of the ignition process in a separated dual-swirl spray flame-Reference-Cited by-同舟云学术

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Experimental investigation of the ignition process in a separated dual-swirl spray flame

Published:2020-09 Issue: Volume:219 Page:161-177
ISSN:0010-2180
Container-title:Combustion and Flame
language:en
Short-container-title:Combustion and Flame

Author:

Yang Siheng,Zhang Chi,Lin Yuzhen,Xue Xin^ORCID,Gan Xiaohua

Funder

National Natural Science Foundation of China

National Science and Technology Major Project

Publisher

Elsevier BV

Subject

General Physics and Astronomy,Energy Engineering and Power Technology,Fuel Technology,General Chemical Engineering,General Chemistry

Reference39 articles.

1. Review of modern low emissions combustion technologies for aero gas turbine engines;Liu;Prog. Aeosp. Sci.,2017

2. Development of the GE aviation low emissions TAPS combustor for next generation aircraft engines;Foust;AIAA 2012-0936,2012

3. Influence of main swirler vane angle on the ignition performance of TeLESS-II combustor;Wang;J. Eng. Gas Turbines Power (ASME),2016

4. Influence of sleeve angle on the LBO performance of TeLESS-II combustor;Wang;AIAA 2016-4693,2016

5. Gas turbine combustion;Lefebvre,1999

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