DESIGN EVALUATION AND IMPROVEMENT OF TJ-24 TURBINE AND PROPELLING NOZZLE BY USING NUMERICAL SIMULATION OF FLUID FLOW
Turbojet TJ-24 is a micro turbojet engine that is made and developed by Mechanical Engineering Department of Institut Teknologi Bandung since 2002. TJ-24 is designed to produce thrust with the amount of 24 N. The main configurations of TJ-24 are intake, KJ66 centrifugal compressor and axial turbine,...
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| Format: | Final Project |
| Language: | Indonesia |
| Online Access: | https://digilib.itb.ac.id/gdl/view/50972 |
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| Institution: | Institut Teknologi Bandung |
| Language: | Indonesia |