
Any thoughts on this as a way to slow down a big plank?
I had a Klingberg Wing 100 that had variable center of gravity. I don’t recall any adverse flight characteristic with the CofG being aft in the landing pattern. In fact I find that the only thing being worse than being tail heavy is being nose heavy. With the CofG being forward the nose would drop prematurely. Meaning that one couldn’t lock in the glide slope. With the result being that landing speeds were far too fast with the subsequent damage from landing too fast. Now what surprised me was that in landing mode (slow flight) I didn’t need to cut down on the aileron throw.* The only Gotcha I recall with the variable CofG was the need to use a servo with a large gear train. I recall using sail and/or retract servos.
What adverse control response should one look out for when moving the CofG aft (narrowing the static margin of stability)on landing? I’m not talking about divergent flight where we would need gyros for flight stability.
* Normally as the CofG is moved aft one needs to cutdown on the control movement. With the CofG moved aft in landing mode this wasn’t required as the aft CofG is only used at low speed. This meant that as the speed built up and the wing started to feel too responsive to the control, it was time to move the CofG forward.
Any thoughts on this as a way to slow down a big plank?