Research Article
Flight Endurance Increasing Technology of New Energy UAV Based on a Strut-Braced Wing
Table 7
The comparison between the SBW and the prototype.
| | Parameters | Prototype | SBW |
| | (m) | 6.31 | 9.2 | | (m) | 0.423 | 0.423 | | 14.918 | 21.749 | | (m2) | 2.669 | 3.892 | | (m) | — | 2.783 | | (m) | — | 0.095 | | (m) | — | 0.121 | | (m) | — | 0.1 | | (m) | — | 0.25 | | (kg) | 22.396 | 21.519 | | 0.685 | 0.785 | | 0.034 | 0.038 | | 20.15 | 20.66 | | (MPa) | 35.654 | 28.567 | | 4.75% | 3.44% | | (W) | 358.15 | 337.156 | | (W) | 295.18 | 346.826 | | (W) | 62.97 | −9.67 |
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