high on carbon
Wing Nut
- Joined
- Dec 29, 2004
- Posts
- 81
- Reaction score
- 6
- Location
- Toronto
As far as I can tell, the wing sails of the AC72's are made of two or more vertical components, which are themselves vertically continuous, kind of like an airplane wing with one or more very large flaps, one behind the other.
I am not aware of these of these components being divided vertically, like the sails on a square rigger, with a mainsail, a top sail, and a top gallant sail. If this were the case, the remedy you mention for being over powered might work
From the pictures I have seen, I can see no such vertical divisions. Correct me if I am wrong.
Or are you saying that each of these two or more vertical components can locally morph its airfoil camber?
Sharpii.
To follow up on an earlier speculation / post you made which I copied above.
Yes that is precisely what wings can do, locally change their camber to the desired shape. Be it on a C-cat or an AC 72, we can 25 degrees of camber at the foot of the wing, perhaps 5 degrees of camber 75% of the way up, and -5 degrees camber at the tip if we wish. additionally on almost all C-cats, and the ETNZ designed wings we can also twist the Main element more than 15 degrees between the foot and the hounds to accommodate twist in AWA due to gradient effects. This allows us to have the desired camber across the entire wing section, and combine that with the desired angle of attack, for any given section of the wing, to match the desired lift characteristics we are after. In short, it's a far more sophisticated approach than can be achieved with soft sails.
In this regard wings can be "bottom loaded" as discussed here, where you put all you drive down low, and therefore reduce your heeling moment, or you match your heeling moment to your righting moment, and take as much thrust down low as you can match to your available side force from your foils, while you flatten off the top of the wing or in some cases invert it, to optimize down wash distribution, the aim being to minimize induced drag from the sail plan.
your observation that the wings are made up of two main elements is correct, but unlike airplane wings, they are not as torsionally stiff as you are imagining. They are designed to be somewhat flexible so they "blow open" then the trimmers can control the amount of twist by limiting it with the control systems. On AC 72's these systems are string and hydraulics. On smaller boats it's pretty much all strings. you cannot see much of the trim systems on contemporary wings as they are mostly buried inside the wing to keep the wing slippery, e.g. low drag.
Additionally some of the flap elements are in fact in separate sections with slip joints between them. as the flap structure twists the leech must grow in length to accommodate the twisting, frequently this is happening at the joints. You cannot see it, because it is subtle, and we tape over the joint to prevent air flowing through the gap. on wings without a straight hinge line, this is especially important to allow the wing to twist correctly and maintain fair curves.
I hope this aids your understanding of how a wing works in mechanical terms.