INTAKE DESIGN FOR INDONESIAN FIGHTER
A research about intake design for Indonesian fighter has been done. The fighter characteristic is flight around Mach 2 at altitude 50,000 feet. This fighter has a rectangular intake configuration with dual ramp using external compression. This research objective is to have the intake configuration...
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| Format: | Theses |
| Language: | Indonesia |
| Online Access: | https://digilib.itb.ac.id/gdl/view/42498 |
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| Institution: | Institut Teknologi Bandung |
| Language: | Indonesia |