Investigation of solid propellant rocket motor nozzle via CFD simulation

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Investigation of solid propellant rocket motor nozzle via CFD simulation

The current work predicts the combustion characteristics of a solid rocket motor especially the flow in the nozzle part. The simulation work is done using computational fluids dynamic (CFD) software. The volume mesh was built in one quarter of the nozzle to reduce time for calculation. The same nozz...

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Bibliographic Details
Main Authors:	Aolin, Chen, A. A., Al Mayas, Abdul Aziz, Faieza, Yidris, Noorfaizal, Ahmad, Kamarul Arifin
Format:	Article
Language:	English
Published:	Akademia Baru Publishing 2020
Online Access:	http://psasir.upm.edu.my/id/eprint/89451/ http://psasir.upm.edu.my/id/eprint/89451/1/ROCKET.pdf

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