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Article information
2004 , Volume 9, Special issue, p.76-81
Zabaikin V.A., Smogolev A.A., Zhapbasbaev U.K., Makashev E.P.
Experimental and numerical modeling of hyperthermal reacting jets structures
Results of experimental and computational modeling of a structure of hyperthermal supersonic reacting jets are presented. Reynolds averaged parabolised Navier-Stokes equations, with turbulence model and multistage mechanism of hydrogen oxidation were used for the numerical algorithm. Problems on wave disturbance propagation and shock waves, dependence of the regularity of ignition and the formation of the flame front on the regime parameters are investigated. The influence of the structure of an airflow on ignition and nature of burnout of a hydrogen, and the temperature influence on the modifications of flame structure are identified.
Author(s):
Zabaikin VA.
Address: 630090, Russia, Novosibirsk
E-mail: lab2@itam.nsc.ru
Smogolev A.A.
Address: 630090, Russia, Novosibirsk
E-mail: lab2@itam.nsc.ru
Zhapbasbaev U K
Address: 480012, Kazakhstan, Almatu
E-mail: nich7@kazsu.kz
Makashev E P
Address: 480012, Kazakhstan, Almatu
E-mail: nich7@kazsu.kz
Bibliography link:
Zabaikin V.A., Smogolev A.A., Zhapbasbaev U.K., Makashev E.P. Experimental and numerical modeling of hyperthermal reacting jets structures // Computational technologies. 2004. V. 9. Special issue. P. 76-81
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