Paper Title :A CFD Analysis & Study On Effect Over Mach Of Rocket C-D Nozzle By Varying Its Geometric Parameters
Author :Nikhil D. Raut
Article Citation :Nikhil D. Raut ,
(2016 ) " A CFD Analysis & Study On Effect Over Mach Of Rocket C-D Nozzle By Varying Its Geometric Parameters " ,
International Journal of Mechanical and Production Engineering (IJMPE) ,
pp. 86-89,
Volume-4,Issue-3
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.
Type : Research paper
Published : Volume-4,Issue-3
DOIONLINE NO - IJMPE-IRAJ-DOIONLINE-4253
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Copyright: © Institute of Research and Journals
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Published on 2016-03-31 |
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