2005
DOI: 10.1063/1.1925149
|View full text |Cite
|
Sign up to set email alerts
|

Analysis of Laser-Generated Impulse In An Airbreathing Pulsed Detonation Engine: Part 1

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1

Citation Types

0
1
0

Year Published

2006
2006
2024
2024

Publication Types

Select...
2
1

Relationship

0
3

Authors

Journals

citations
Cited by 3 publications
(1 citation statement)
references
References 3 publications
0
1
0
Order By: Relevance
“…The parabolic afterbody acts as both a primary receptive optic for the incident laser beam, and an expansion nozzle for the heated exhaust flow. Current research into lightcraft inlet designs is somewhat limited, with the typical configurations being similar to that of the Lightcraft Technology Demonstrator concept [3]. This research aims to investigate and extend the work on hypersonic lightcraft inlets to provide a stable and efficient platform for the pulsed laser detonation engine.…”
Section: Introductionmentioning
confidence: 99%
“…The parabolic afterbody acts as both a primary receptive optic for the incident laser beam, and an expansion nozzle for the heated exhaust flow. Current research into lightcraft inlet designs is somewhat limited, with the typical configurations being similar to that of the Lightcraft Technology Demonstrator concept [3]. This research aims to investigate and extend the work on hypersonic lightcraft inlets to provide a stable and efficient platform for the pulsed laser detonation engine.…”
Section: Introductionmentioning
confidence: 99%