2018
DOI: 10.1088/1742-6596/946/1/012066
|View full text |Cite
|
Sign up to set email alerts
|

Laser-induced breakdown ignition in a gas fed two-stroke engine

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1

Citation Types

0
1
0

Year Published

2018
2018
2019
2019

Publication Types

Select...
5

Relationship

0
5

Authors

Journals

citations
Cited by 7 publications
(1 citation statement)
references
References 9 publications
0
1
0
Order By: Relevance
“…Flight safety and sustainability of the propulsion systems in aerospace engineering are strongly linked to the ignition technology and combustion control. The propulsive performance of air-breathing pulse detonation engiones (PDEs) has been theoretically and numerically studied over a wide range of system configurations, operating parameters and flight conditions [1,2], and various ignition systems (e.g., electric discharge, microwave discharge, laser radiation, laser-induced breakdown) have been tested to achieve simultaneous space ignition via multiple ignition points throughout the combustion chamber [3][4][5][6][7][8].…”
Section: Introductionmentioning
confidence: 99%
“…Flight safety and sustainability of the propulsion systems in aerospace engineering are strongly linked to the ignition technology and combustion control. The propulsive performance of air-breathing pulse detonation engiones (PDEs) has been theoretically and numerically studied over a wide range of system configurations, operating parameters and flight conditions [1,2], and various ignition systems (e.g., electric discharge, microwave discharge, laser radiation, laser-induced breakdown) have been tested to achieve simultaneous space ignition via multiple ignition points throughout the combustion chamber [3][4][5][6][7][8].…”
Section: Introductionmentioning
confidence: 99%