Calculate max load factor of plane formula
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In aeronautics, the load factor is defined as the ratio of the lift of an aircraft to its weight[1][2]:§ 5.22 and represents a global measure of the stress ("load") to which the structure of the aircraft is subjected:
{\displaystyle n={\frac {L}{W}}}
where:
n = Load factorL = LiftW = Weight
{\displaystyle n={\frac {L}{W}}}
where:
n = Load factorL = LiftW = Weight
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