PERANCANGAN TURBIN AKSIAL SATU TINGKAT UNTUK MESIN TURBOJET KECIL
This paper explains about aerodynamic design of a single stage gas generator turbine for a small turbojet engine. The design requirement is that the turbine must be able to deliver power output of 150 kW at 0.814 kg/s gas mass flow, with turbine inlet temperature of 1200 K, and turbine inlet pressur...
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| Format: | Final Project |
| Language: | Indonesia |
| Online Access: | https://digilib.itb.ac.id/gdl/view/33890 |
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| Institution: | Institut Teknologi Bandung |
| Language: | Indonesia |