Study of gas flows about the air inlet of high-speed flying vehicles

Flowfields of various gasodynamic parameters at high supersonic flows about the air intakes of flying vehicles are analyzed. Mathematical model of high supersonic flows is set and verified. Numerical simulation of perfect gas flow in non-profiled ducts of air intakes is provided. Various methods of multicomponent mixture simulation are used. Influence of flow multi-componence of shock waves near the head of flying vehicle is considered.