An aircraft with a Centre of Gravity towards the aft limit will experience what change in range and stalling speed?

When an aircraft's center of gravity is positioned towards the aft limit, the effects on range and stalling speed can be understood through fundamental aerodynamic principles.

Having a rearward center of gravity results in the aircraft being generally more stable during straight and level flight. This stability allows the aircraft to maintain a more efficient flight profile, potentially leading to an increased range. The aerodynamic forces acting on the aircraft are optimized, reducing drag during cruise flight. Thus, with efficient lift-to-drag ratios, the aircraft can fly further on the same amount of fuel.

Additionally, a more aft center of gravity can lead to a decrease in stalling speed. This is because an aft center of gravity allows the aircraft to achieve a higher angle of attack before reaching the critical state at which it stalls. As a result, the aircraft can fly at lower speeds before transitioning into a stall condition. This does not mean that the aircraft becomes “safer” at all speeds; the characteristics are simply altered.

Therefore, an aircraft with a center of gravity towards the aft limit experiences an increased range and a decreased stalling speed, reflecting the aerodynamic advantages provided by this specific weight distribution.