Hamza, Bakdam Khoirul (2019) Analisa Kinerja Military Turbofan Engine F100-PW-220 Pada Pesawat Tempur F-16 A/B. Diploma thesis, Institut Teknologi Sepuluh Nopember.
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Abstract
Military Turbofan engine merupakan sistem pemebangkit daya yang beroperasi berdasarkan Siklus Brayton. Hasil dari Siklus Brayton ini berupa gaya dorong yang digunakan untuk pesawat terbang. Dalam menghasilkan daya dorong menggunakan hitungan termodinamika dan mekanika fluida yang menggunakan compressible flow, local isentropic stangtion propertis untuk mengetahui tiap state.
Degan mengetahui tiap state kita bisa mengethaui performa dari engin, yang berupa thrust dan spesific feul consumption (SFC). Pada Tugas Akhir ini dilakukan perhitungan performa sebelum dan sesudah perawatan.
Berdasarkan hasil perhitungan diperoleh kenaikan thrust 5854,9248 N dan penurunan SFC sebesar 0,0254 dari kondisi idle sebelum perawatan ke susudah perawatan. Sedangkan pada kondisi mill menghasilkan thrust sebesar 65117,5052 N dan SFC sebesar 0,0013. Dengan kondisi ABMAX menghasilkan thrust sebesar 146681,6418 N dan SFC 0,0006.
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Military Turbofan engine is a power generating system that operates based on the Brayton Cycle. The result of this Brayton cycle is the thrust used for aircraft. In producing thrust using thermodynamics and fluid mechanics that use compressible flow, local isentropic stagnation properties to determine each state.
By knowing each state we can know the performance of engine, which is in the form of thrust and specific feul consumption (SFC). In this Final Project, the performance of before and after treatment is calculated.
Based on the calculation results obtained an increase in thrust 5854,9248 N and a decrease in SFC of 0.0254 from idle conditions before treatment to the next treatment. Whereas in mill conditions it produces thrust of 65117.5052 N and SFC of 0.0013. With conditions ABMAX produces thrust of 146681,6418 N and SFC 0,0006.
| Item Type: | Thesis (Diploma) |
|---|---|
| Additional Information: | RSMI 629.134 353 Ham a-1 2019 |
| Uncontrolled Keywords: | Military Turbofan engine, Thrust, SFC |
| Subjects: | U Military Science > UG1242 Drone aircraft--Control systems. (unmanned vehicle) |
| Divisions: | Faculty of Vocational > Mechanical Industrial Engineering (D4) |
| Depositing User: | Hamza Bakdam Khoirul |
| Date Deposited: | 02 Jan 2024 02:27 |
| Last Modified: | 02 Jan 2024 02:27 |
| URI: | http://repository.its.ac.id/id/eprint/70222 |
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