OPTIMIZATION OF THERMAL BARRIER COATING APPLICATION PARAMETERS ON F-16 JET ENGINE EXHAUST NOZZLE COMPONENTS WITH PLASMA SPRAY METHOD
Thermal barrier coating (TBC) is a crucial part of jet engine components including the exhaust nozzle of the F-16 fighter jet. The TB portion of this component will be damaged with use. For this reason, this study was conducted to determine the optimum spraying distance and feed rate parameters in m...
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| Format: | Final Project |
| Language: | Indonesia |
| Online Access: | https://digilib.itb.ac.id/gdl/view/67269 |
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| Institution: | Institut Teknologi Bandung |
| Language: | Indonesia |
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