Lift required is maximum at the bottom of the loop calculator

At the bottom of the loop, the aircraft is usually experiencing maximum positive G-forces (acceleration) pushing the pilot and the aircraft downward. The lift force provided by the wings must counteract the increased weight due to these G-forces, along with the aircraft’s normal weight. 

L means lift required is maximum at the bottom of the loop

W means weight 

V means velocity

Gr means gravity

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