DESIGN PROCESS, MANUFACTURE, AND TESTING OF PROPELLER FOR HIGH ALTITUDE LONG ENDURANCE UAV
The HALE UAV which developed at the Bandung Institute of Technology has a design requirements and objectives to cruise at an altitude of 60,000 ft with cruising speed of 22.1 m/s and propeller rotational speed of 3400 RPM. The designed “basic” propeller using Larrabee – CFD corrected method has been...
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| Format: | Theses |
| Language: | Indonesia |
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| Online Access: | https://digilib.itb.ac.id/gdl/view/72869 |
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| Institution: | Institut Teknologi Bandung |
| Language: | Indonesia |
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