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...
| Main Authors: | , , , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Akademia Baru Publishing
2020
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| Online Access: | http://psasir.upm.edu.my/id/eprint/89451/1/ROCKET.pdf |