Effect of a head geometry structure on the ignition performance of a combustor-Reference-Cited by-同舟云学术

Effect of a head geometry structure on the ignition performance of a combustor

Published:2022-04 Issue: Volume:123 Page:107428
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Li Wei,Di Dong,Liu Yunpeng,Tian Zemin,Yan Yingwen

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference28 articles.

1. Analysis on influences of plateau condition on starting performance of turbofan engine;Miao;Eng. Test,2016

2. Ignition dynamics of an annular combustor equipped with multiple swirling injectors;Bourgouin;Combust. Flame,2013

3. Division method of aero-engine flight envelope area;Lian;Int. Combust. Eng. Parts,2020

4. Ignition and flame quenching of flowing heterogeneous fuel-air mixtures;Ballal;Combust. Flame,1979

5. Experimental study on blowout characteristics of aeroengine combustor under high altitude low pressure and low-temperature condition;Guangming;Phys. Gases,2019

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