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Statistics report
Dec. 2022
Submitted Papers : 80
Accepted Papers : 10
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Acc. Perc : 12%
Issue Published : 113
Paper Published : 2211
No. of Authors : 6284
  Journal Paper


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


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