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This final project performed the optimization of reverse combustion chamber design of 500 N turbojet engine static thrust by using a 2D axisymmetric CFD method. Optimization of reverse combustion chamber design done because the first generation 500 N turbojet engine that has been manufactured and te...
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| Format: | Final Project |
| Language: | Indonesia |
| Online Access: | https://digilib.itb.ac.id/gdl/view/16503 |
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| Institution: | Institut Teknologi Bandung |
| Language: | Indonesia |
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