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HERO ID
6183862
Reference Type
Journal Article
Title
Combustion properties of gaseous CH4/O2 coaxial jet flames in a single-element combustor
Author(s)
Choi, S; Jeung, IS; Kim, HK; Kim, TY; Koo, J; Kwon, OC
Year
2016
Is Peer Reviewed?
1
Journal
Fuel
ISSN:
0016-2361
EISSN:
1873-7153
Volume
184
Page Numbers
28-35
DOI
10.1016/j.fuel.2016.07.001
Web of Science Id
WOS:000381619800004
URL
http://www.sciencedirect.com/science/article/pii/S0016236116305968
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Abstract
Fundamental combustion properties of gaseous methane (CH4)/oxygen (O2) coaxial jet flames in a single-element combustor are experimentally evaluated as a preliminary step for subsequent studies of injection at very low temperature or using liquid O2 for CH4/O2 bipropellants, recently appearing to be the oncoming liquid bipropellant. A combustion chamber with quartz windows, a single shear coaxial injector and an exhaust nozzle on the downstream of the chamber is considered for the present study. Focusing on the measurements of the ignition and combustion stability limits of the coaxial jet flames in the chamber, flame visualization is also conducted by OH∗ chemiluminescence, schlieren imaging and direct imaging. Results show the ignition limits restricted than the combustion stability limits. Flame behaviors are largely classified into two, the stably attached flame and the oscillating, liftoff (near-blowout) flame. Due to cooling effects on the wall of the chamber, stably liftoff flame is not observed. The stability of the flame is greatest at fuel-rich condition (based on the injected amounts of CH4 and O2). From the flame visualization flame thickness is found to be smaller than the injector lip thickness and insensitive to injection conditions. The laminar-flow behavior near the injector exit due to the strong burning of pure O2 is observed even for high Reynolds numbers (Re). The flame visualization also exhibits the recirculating O2 that enhances burning in the combustor through the reaction with the outer fuel jet. The results of ignition limits, combustion stability limits and flame visualization can be used as a database for researches of modeling the gaseous CH4/O2 jet flames in the combustion chamber.
Keywords
Methane; Bipropellants; Ignition limits; Combustion stability limits
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