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<br /> <p align="justify">This tubular & reverse-flow annular combustion chambers are designed for gas turbine simulator system. Combustion chamber is positioned between compressor and turbine. Combustion chamber is designed to increase enthalpy without significant pressur...
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| Format: | Final Project |
| Language: | Indonesia |
| Online Access: | https://digilib.itb.ac.id/gdl/view/27189 |
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| Institution: | Institut Teknologi Bandung |
| Language: | Indonesia |