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Beschreibung
This book uncovers design considerations for an inlet of a split-wing, electric distributed propulsion aircraft. The purpose of this document is to demonstrate the effectiveness of the split-wing design for electric an hybrid-electric systems. It is still unknown whether the split-wing system is competitive compared to 'over-wing' and 'under-wing' configurations. Further investigation is required to better understand these new aircraft configurations.
Details
| Verlag | LAP LAMBERT Academic Publishing |
| Ersterscheinung | 23. Juli 2015 |
| Maße | 22 cm x 15 cm x 0.7 cm |
| Gewicht | 161 Gramm |
| Format | Softcover |
| ISBN-13 | 9783659761461 |
| Seiten | 96 |