Rapor Design

Design Constraints
Wing Area ( Load is considered)
Wing Span (
Airfoil ( lift, drag, weight) ( Istanbul’s conditions were also considered such as density, weather conditions) (lift to drag ratio)
Fuselage Size
Tail Size ( Horizontal and Vertical, depending on the weight and CoG)
Motor Selection ( Power, Efficiency)
Battery Selection ( Light, efficient)
Speed Controller Selection
Propeller Section(Up to 40 Ampers, as light as possible, low voltage consumption)
Track Regime
Sizing Parameters; Aspect Ratio, Max Payload Weight, Empty Weight, Battery Weight, Takeoff Weight for all missions

Airfoil Selection