Load factor
The ratio of the load supported by the wings to the actual weight of the aircraft, expressed in g. Load factor rises in turns and pull-ups (about 2 g in a 60° bank level turn) and raises the stall speed.
Related terms
The ratio of the load supported by the wings to the actual weight of the aircraft, expressed in g. Load factor rises in turns and pull-ups (about 2 g in a 60° bank level turn) and raises the stall speed.