Analysis and Initial Optimization of The Propeller Design for Small, Hybrid-Electric Propeller Aircraft
This thesis focuses on the optimization of the electric aircraft propeller in order to increaseflight performance. Electric aircraft have limited energy, particularly the electricmotor torque compared to the fuel engine torque. For that, redesign of the propeller forelectric aircraft is important in...
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| Format: | Others |
| Language: | English |
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KTH, Flygdynamik
2020
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| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-287726 |