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OH PLIF Visualization of the UVa Supersonic Combustion Experiment: Configuration A

Authors :
Luca M. L. Cantu
Andrew D. Cutler
Emanuela C. A. Gallo
Christopher P. Goyne
Colin D. McRae
James C. McDaniel
Paul M. Danehy
Robert D. Rockwell
Craig T. Johansen
Gaetano Magnotti
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.

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