CFD Analysis of Co-Axial Dual Compressible Jets
In this thesis, a dual coaxial nozzle will be designed and modeled in Pro/Engineer. CFD analysis will be done by
considering three important parameters, such as pressure ratios of the inner and outer nozzles, and outer nozzle ejection
angle, for a better understanding of jet structures. Analysis will be done in Ansys. Analysis will be performed by varying exit
velocity ratios. The outputs determined will be mach number, Reynold’s number, pressure drop.