THERMAL BARRIER COATING AMDRY 962 AND METCO 204 NS WITH PLASMA SPRAY METHOD FOR F16 AIRCRAFT EXHAUST NOZZLE APPLICATION
The exhaust nozzle acts as a propulsion generator to help the aircraft maintain speed and operate under aggressive environments at high temperatures of around 900 °C to 1100 °C with turbine engine operating hours of nearly 50,000 hours and repeated. The nozzle converts the potential energy from the...
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| 格式: | Theses |
| 語言: | Indonesia |
| 在線閱讀: | https://digilib.itb.ac.id/gdl/view/67121 |
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| 機構: | Institut Teknologi Bandung |
| 語言: | Indonesia |