Investigation of the Nonequilibrium Viscous Shock Layer on a Catalytic Surface with Conjugate Heat Exchange
Nonequilibrium dissociated air flow problem at stagnation region for the aerodynamic reentry trajectory. The hypersonic viscous shock layer theory (TVSL) including nonequilibrium chemical reactions, multicomponent diffusion is used as initial mathematical model. On the body surface the nonstationary conjugate heat transfer is taken into the account. High order numerical approach is suggested. Some numerical results are presented
Issue: 6, 2004
Series of issue: Sciences
Rubric: Applied Mechanics
Pages: 59 — 64
Downloads: 963