Going on what John Farley has just emailed me(agreeing with Genghs) the clue is in the fact that no aircraft can turn without a turning force.
So I would say then we are still talking about an increase in loading because there must be a centre seeking force which in turn must increase the loading.
In relation to a full power climbing turn stall in a SE prop A/C, surely there must be a RAF difference due to slipstream over the roots but is that equal over both roots in a balanced climbing turn?
Last edited by Pull what; 15th May 2012 at 13:12.