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Article information
2007 , Volume 12, Special issue, p.17-25
Beketaeva A.O., Naimanova A.Z.
Application of ENO (essentially nonoscillatory) scheme to modeling of multi-component flows
This paper addresses a numerical investigation of the plane supersonic turbulent multi-component flow with the perpendicular injection of a hydrogen from the slots located symmetrically on the lower and the upper walls of a channel. For the mathematical modeling of such flows the full Navier - Stokes equation for multi-component flow fields were used. On the basis of the ENO-scheme the computational code has been developed. We study the influence of the Mach number on the length of separation region and the penetration depth of a hydrogen jet into a supersonic air crossflow.
[full text] Author(s):
Beketaeva A.O.
Address: Kazakhstan, Almatu
E-mail: KED@math.kz
Naimanova A Zh
Address: Kazakhstan, Almatu
E-mail: KED@math.kz
Bibliography link:
Beketaeva A.O., Naimanova A.Z. Application of ENO (essentially nonoscillatory) scheme to modeling of multi-component flows // Computational technologies. 2007. V. 12. Special issue 4. P. 17-25
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