Paper Title
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.