Effects of airstream Mach number on H2/N2 plasma igniter

Journal of Propulsion and Power

Volumn 18, Issue 3, 2002, Pages 679-685

  Masuya, Goro ^a   Takita, Kenichi ^a   Takahashi, Katsuyoshi ^a   Takatori, Fumio ^a   Ohzeki, Hiroyuki ^a  

^a TOHOKU UNIVERSITY   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; COMBUSTION; FEEDSTOCKS; HYDROGEN FUELS; PLASMA TORCHES; PLASMAS; PRESSURE EFFECTS;

PLASMA IGNITERS;

IGNITION SYSTEMS;

EID: 0036575896     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/2.5984     Document Type: Article

References (17)

1. Autoignition of hydrogen injected transverse to supersonic airstream
2. Supersonic combustion of propane
3. Use of silane in scramjet research
4. The use of a plasma jet for flame stabilization and promotion of combustion in supersonic air flows
5. Development and evaluation of a plasma jet flameholder for scramjets
6. Some governing parameters of plasma torch igniter/flame-holder in a scramjet combustor
7. Scramjet engine tests at mach 4 and 6
8. Asymptotic analysis of plasma jet igniter
9. Ignition characteristics of plasma torch for hydrogen jet in airstream
10. Three dimensional numerical simulation of combustion of hydrogen jet with plasma torch
11. Mach 6 testing of a scramjet engine model
12. Ignition of parallel and low-angle hydrogen jet by plasma torch
13. Effectiveness of plasma torches for ignition and flameholding in scramjet
14. Thermal efficiency of plasma torch igniter
15. Effect of plasma torch feedstock on ignition characteristics in supersonic flow
16. Chemical kinetics and self-ignition in a model supersonic hydrogen-air combustor
17. Operating characteristics of a hydrogen-argon plasma torch for supersonic combustion applications