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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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Bibliographic Details
Main Author: SITIO (NIM : 136 06 040); Pembimbing Dr. Firman Hartono, MOSES
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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