Minimum length rocket engine nozzle using method of characteristics as a function of exit Mach number, number of characteristics and inlet diameter. It also generates mesh for convergent-divergent nozzle where convergent part is added.
Minimum length rocket engine nozzle using method of characteristics as a function of exit Mach number, number of characteristics and inlet diameter. It also generates mesh for convergent-divergent nozzle where convergent part is added.