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Inlet Distortion Effects on Fuel Distribution and Ignition in Scramjet Cavity Flameholder
- Source :
- Journal of Propulsion and Power. 35:601-613
- Publication Year :
- 2019
- Publisher :
- American Institute of Aeronautics and Astronautics (AIAA), 2019.
-
Abstract
- The effects of inlet distortion and shockwave interaction on fuel-air distribution and ignition in a cavity-based flameholder with supersonic flow were investigated using nanosecond-gated laser-ind...
- Subjects :
- 020301 aerospace & aeronautics
Materials science
Mechanical Engineering
Aerospace Engineering
02 engineering and technology
Mechanics
01 natural sciences
010305 fluids & plasmas
law.invention
Ignition system
Boundary layer
Fuel Technology
0203 mechanical engineering
Space and Planetary Science
law
0103 physical sciences
Oblique shock
Scramjet
Laser-induced breakdown spectroscopy
Inlet distortion
Choked flow
Wind tunnel
Subjects
Details
- ISSN :
- 15333876 and 07484658
- Volume :
- 35
- Database :
- OpenAIRE
- Journal :
- Journal of Propulsion and Power
- Accession number :
- edsair.doi...........f4ade954cdb886c4a6aece52791735c3
- Full Text :
- https://doi.org/10.2514/1.b37204