Estudo analítico/numérico do problema de ablação em corpos rombudos com simetria axial

Coordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES)

Combustão do hidrogênio em escoamento supersônico

This work investigated the operating conditions of a 'scramjet' through numerical simulation considering two-dimensional steady flow. Using a commercial software, FLUENT, cases of inviscid flow with and without fuel injection, turbulent flow without fuel injection, turbulent flow with fuel injection and without burning, and finally turbulent flow with fuel injection and burning are simulated