Chemical nonequilibrium general computational software design of nozzle one dimensional flow field

The general computational software of rocket engine one dimensional nozzle nonequilibrium flow, which is based on a unified chemical library, can simulate the flow field of rocket engine nozzle with the propellants consisted of carbon, hydrogen, oxygen, nitrogen, fluorine, and chlorine elements. By computing the nozzle flow field with the propellant elements of hydrogen, oxygen and carbon, hydrogen, oxygen, nitrogen, the fields of velocity, temperature, pressure and all species mass fraction were gotten, which can be used as reference for designer.