Numerical investigation of the ramjet and scramjet operation regimes of the HIFiRE-2 combustion chamber

DOI10.1134/S0015462822601164OpenAlexW4310239179MaRDI QIDQ2107833

R. K. Seleznev

Publication date: 5 December 2022

Published in: Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1134/s0015462822601164

zbMATH Keywords

effective diffusion coefficientAUSM explicit finite difference schemekinetic combustion diagramMach number distributionmulticomponent Navier-Stokes equations

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Combustion (80A25) Reaction effects in flows (76V05) Compressible Navier-Stokes equations (76N06)

Cites Work

• Unnamed Item
• Three-dimensional problem of radiative gasdynamics of the Apollo-4 command module during superorbital atmospheric entry

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