There is no more stiffness to be had that affects rotor blade sailing/flapping after reaching 60 to 100 rotor RPM. Blade sail or flap is not caused by lack of centrifugal force. It is caused due to aerodynamic reasons as a retreating blade stall due to dissymmetry of lift and that has no bearing cetrifugal/petal force. That part of the ground explanation is not technically correct and too casual. Also, I believe what he is trying to say is that you balance on the mains after starting with stick full aft and takeoff and build speed before allowing it to climb without getting behind the power curve.