Modelling and Computational Fluid Dynamic Analysis on Jet
The jet nozzle can take three different materials like Titanium Tungsten and Nickel It can observe the material is to be in the supersonic flow in the nozzle The Mach number at the nozzle exit is observed to be less in comparison with designed value This is due to the viscosity and turbulence in fluid near the wall of the duct The Mach number decreases due to shock wave and reversible