DOIONLINE 
DOIONLINE Publish In |
International Journal of Mechanical and Production Engineering (IJMPE)-IJMPE |
 Journal Home Volume Issue |
||||||||
Issue |
Volume-4,Issue-3 ( Mar, 2016 ) | |||||||||
Paper Title |
A CFD Analysis & Study On Effect Over Mach Of Rocket C-D Nozzle By Varying Its Geometric Parameters | |||||||||
Author Name |
Nikhil D. Raut | |||||||||
Affilition |
UG Student, Department of Mechanical Engineering, BNCOE, PUSAD. | |||||||||
Pages |
86-89 | |||||||||
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. | |||||||||
| View Paper | ||||||||||
