SHOULDER (GULL) WING VTOL first layout
grabcad
Initially, the layout design appeared promising, with the aim of reducing wingspan by utilizing air from propellers to provide extra lift on the wing's lower side. Additionally, a combination of two free rotors and 90mm EDF offered approximately 20% more lift than the estimated weight for this configuration. However, upon creating detailed sketches, several flaws were identified. Some could be corrected, but others couldn't. Ultimately, the configuration was rejected.
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