Problem Statement | Build a lightweight and aerodynamically efficient Aerobody |
Goals | Aerodynamic efficiency will lead to reduced power requirements, this allows us to travel further with the same amount of power. |
Constraints Regulations | Top surface area of 5m^2 to accomodate array (If curved, then only in 1 plane) Max dimensions (L x W x H): 5.0m x 2.2m x 1.6m |
Criteria | Theoretical Coefficient of drag (Cd) < 0.1 Frontal area (A) < 1.2 m2 Large enough to accommodate 1 person |
Requirements | Minimize molds Minimize cost Highly durable |
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