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OH PLIF Visualization of the UVa Supersonic Combustion Experiment: Configuration A
- Source :
- 28th Aerodynamic Measurement Technology, Ground Testing, and Flight Testing Conference.
- Publication Year :
- 2012
- Publisher :
- American Institute of Aeronautics and Astronautics, 2012.
-
Abstract
- Hydroxyl radical (OH) planar laser-induced fluorescence (PLIF) measurements were performed in the University of Virginia supersonic combustion experiment. The test section was set up in configuration A, which includes a Mach 2 nozzle, combustor, and extender section. Hydrogen fuel was injected through an unswept compression ramp at two different equivalence ratios. Through the translation of the optical system and the use of two separate camera views, the entire optically accessible range of the combustor was imaged. Single-shot, average, and standard deviation images of the OH PLIF signal are presented at several streamwise locations. The results show the development of a highly turbulent flame structure and provide an experimental database to be used for numerical model assessment.
- Subjects :
- Flow visualization
Materials science
business.industry
Turbulence
Flame structure
Nozzle
Condensed Matter Physics
Combustion
symbols.namesake
Optics
Mach number
Aeronautics
Planar laser-induced fluorescence
symbols
Combustor
Scramjet
Supersonic speed
Electrical and Electronic Engineering
Combustion chamber
business
Subjects
Details
- Database :
- OpenAIRE
- Journal :
- 28th Aerodynamic Measurement Technology, Ground Testing, and Flight Testing Conference
- Accession number :
- edsair.doi.dedup.....db3b723e8af886f7a3eff3c3e7620444
- Full Text :
- https://doi.org/10.2514/6.2012-2887