Spray and Combustion Modeling in High Pressure Cryogenic Jet Flames
Keyword(s):
The aim of the present work is the investigation of the combustion phenomenon in liquid-propellant rocket engines. The combustion of liquid oxygen and gaseous methane in a shear coaxial injector under supercritical pressure was analyzed. To realize an efficient numerical description of the phenomena, it is important to treat the LOx jet in a manner which takes into account its real behavior. In the present work different kinetics, combustion models and thermodynamics approaches were used in association with the description of the jet as a discrete phase. For all the approaches used, a comparison with experimental data from literature was performed.
1967 ◽
Vol 4
(12)
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pp. 1569-1580
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2019 ◽
Vol 107
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pp. 63-84
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Keyword(s):
1960 ◽
pp. 183-215
Keyword(s):