Paper Title
A CFD Analysis & Study On Effect Over Mach Of Rocket C-D Nozzle By Varying Its Geometric Parameters

Abstract
CFD analysis of Rocket engine nozzle has be conducted to study the effect over Mach number by varying Convergent-Divergent (CD) nozzle geometric parameters such as providing curvature at throat section, varying inlet, outlet & throat diameter and changing length of divergent section by using ANSYS Fluent Workbench 16.0. And it is found that every CD nozzle shows good result in this limit. Keywords- Rocket, Convergent- Divergent Nozzle, Mach, CFD.