UAV Design Assembly
grabcad
The UAV design entails a 15-part assembly featuring simplified boxes for payload assessment and determination of mass property alterations due to diverse configurations. Subsequent testing encompasses wing spar evaluation and running computational fluid dynamics simulations to analyze how the downwash from the wing influences tail lift coefficient. Notably, the horizontal stabilizer is positioned lower than the wing, a rarity in aircraft design, so it will be intriguing to study the impact of the wing's wake on the stabilizer performance.
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