We consider two dimensional steady state inviscid flow of air around flying objects including chemical reactions. We present the result of numerical computations of nonequilibrium hypersonic inviscid flow of low density. The model problem is based on ...
We consider two dimensional steady state inviscid flow of air around flying objects including chemical reactions. We present the result of numerical computations of nonequilibrium hypersonic inviscid flow of low density. The model problem is based on the Euler equations and a chemical reaction model accounting for the finite rate reactions. We obtained detailed detailed description of flow properties near the shock and body.