Numerical research on mixing characteristics of different injection schemes for supersonic transverse jet

DOI10.1007/S11431-010-4277-9zbMath1237.76065OpenAlexW1966280549MaRDI QIDQ412814

ZhenXun Gao, Chun Hian Lee

Publication date: 4 May 2012

Published in: Science China. Technological Sciences (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s11431-010-4277-9

zbMATH Keywords

numerical simulationsupersonic mixinginjection schememixing efficiency

Mathematics Subject Classification ID

Navier-Stokes equations for incompressible viscous fluids (76D05) (k)-(varepsilon) modeling in turbulence (76F60) Supersonic flows (76J20)

Related Items (2)

Overset structured grids assembly method for numerical simulations of multi-bodies and moving objects ⋮ Application and theoretical analysis of the flamelet model for supersonic turbulent combustion flows in the scramjet engine

Uses Software

• CHEMKIN

Cites Work

• A numerical study of turbulent combustion characteristics in a combustion chamber of a scramjet engine
• Towards the ultimate conservative difference scheme. V. A second-order sequel to Godunov's method
• An Accurate and Robust Flux Splitting Scheme for Shock and Contact Discontinuities
• Unnamed Item

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