Computes the load factor (g-force) in a coordinated level turn at a given
bank angle. Load factor increases with bank angle because the vertical
component of lift must still support the aircraft's weight while the
horizontal component provides centripetal force.
At 0 degrees bank, load factor is 1g (straight and level).
At 60 degrees, it is 2g. At 75 degrees, approximately 3.86g.
Computes the load factor (g-force) in a coordinated level turn at a given bank angle. Load factor increases with bank angle because the vertical component of lift must still support the aircraft's weight while the horizontal component provides centripetal force.
At 0 degrees bank, load factor is 1g (straight and level). At 60 degrees, it is 2g. At 75 degrees, approximately 3.86g.