ANALISIS NUMERIK PENGARUH KONFIGURASI LUBANG LINER TERHADAP PERFORMA RUANG BAKAR MESIN TURBIN BERUKURAN KECIL
In this final project the author discusses about numerical analysis of four combustion chamber models that will be considered to be used for gas turbine engine. These models are tubular combustion chamber with curved vane swirler as a flame stabilization method. Curved vane swirler is used in order...
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| Main Author: | |
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| Format: | Final Project |
| Language: | Indonesia |
| Online Access: | https://digilib.itb.ac.id/gdl/view/53901 |
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| Institution: | Institut Teknologi Bandung |
| Language: | Indonesia |