| Issue |
MATEC Web Conf.
Volume 115, 2017
XXXIII Siberian Thermophysical Seminar (STS-33)
|
|
|---|---|---|
| Article Number | 03010 | |
| Number of page(s) | 4 | |
| Section | Chapter 3 Transport processes in physical and chemical transitions, including combustion | |
| DOI | https://doi.org/10.1051/matecconf/201711503010 | |
| Published online | 10 July 2017 | |
Experimental investigation of open cavity as flame holder of supersonic combustor
ITAM SB RAS, 4/1 Institutskaya, Novosibirsk, 630090, Russia
* Corresponding author: gold@itam.nsc.ru
The results of a study of combustion stabilization in a supersonic combustor for Mach numbers 2, 2.5, and 3 are presented. It was shown that the choice of the fuel injection scheme has decisive influence on the mixing efficiency and flame holding. It has been established that the efficiency of combustion stabilization depends essentially on Mach number and total temperature at the channel entrance.
© The Authors, published by EDP Sciences, 2017
This is an Open Access article distributed under the terms of the Creative Commons Attribution License 4.0, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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