I love Ted's description of how adding tip weight increases line tension because the resultant hinging, vectors the lift away from the pilot. Now follow me as I describe a hypothetical case.
If I add tip weight ,to get line tension, then I add a wart to get rid of the hinging that results , What have I actually gained? Perhaps just a heavier plane and a stylish wart.Is there some way that the added tip weight helps line tension apart from the hinging/vectoring process. Keith Varley
Hi Keith,
Bet you thought you got me with that one, didn't you!
Loss of line tension is often (usually) associated with a loss in speed. We try to avoid it as much as possible but it does happen despite all of our efforts. When the CG is displaced spanwise from the
thrust line there is a moment produced between the two whenever the airplane accelerates. Thus the further outboard of the thrust line the CG is located the greater that moment will be to direct the airplane toward the end of the lines restoring the tension lost when the airplane slowed down. One of the biggest reasons that equal panel wings are very popular is because they require a goodly amount of tip weight to counteract the higher speed of the outboard panel. That weight moves the CG outboard from the thrust line which is helpful not only in helping with line tension in maneuvers but also has a dramatic effect on the ability to maintain line tension during the launch on windy days.
The greatest acceleration the ship ever experiences is right at launch. With the CG outboard Mother Nature provides additional tension during the launch when there is little or no pull on the lines due to centrifugal force. The CG wants to lag behind the thrust line which will cause some yaw to the right creating tension. In addition, the yaw to the right vectors the thrust away from the pilot thus compounding the effect.
It's a really good idea to have the CG outboard of the thrust line and if you utilize a longer inboard wing it is worth paying attention to.
With the CG
inboard of the thrust line the opposite effect takes place and can be quite disturbing. Think of an All American, Sr on takeoff and its well earned reputation for wanting to come in on the pilot. Because the AA, Sr. has that three inch longer inboard wing to get it properly balanced for flight the spanwise CG has to be somewhat inboard of the thrustline. The net effect of that is an inward yaw on take off that can be truly disturbing. The only appropriate fix for the AA, Sr. built to spec is to offset the engine enough that the thrust line (from the top view) passes through or inboard of the CG.
It's a real effect and well worth considering in the design or trim phase. I use some wing assymetry in all of my designs but am opposed to significant engine offset. As a result many if not most of my "serious" stunt ships end up with the wart.
Anyway, I think that's right.

Ted