Doug Lord
Flight Ready
- Joined
- May 26, 2009
- Posts
- 16,679
- Reaction score
- 354
- Location
- Cocoa, Florida
Moth on Foils!----The Wing
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As an anonoymous participant here your are free to say whatever you want to with no fear of being held accountable.
If you read what Steve Clark has said or particularly what Adam May has said(and done)-both very experienced with wings-you would realize that, at best,
your analysis of the wings for the Moth is flawed. It really wouldn't take you very long to read the material.....
Posts: 1134(May standing on immersed wing, 1136(Steve Clark) and last but not least 1138(Adam May on transport, cost and ruggedness).
* Not in the A Class and not known for sure in the Moth class(so far)
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From Tom Speer:
Mr. Haines:
Wings are fragile, witness Team USA's $4-500,000 worth of C Class breakage this year on two days sailing. Wings are stunning performers.*
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CutOnce
--------------------------
As an anonoymous participant here your are free to say whatever you want to with no fear of being held accountable.
If you read what Steve Clark has said or particularly what Adam May has said(and done)-both very experienced with wings-you would realize that, at best,
your analysis of the wings for the Moth is flawed. It really wouldn't take you very long to read the material.....
Posts: 1134(May standing on immersed wing, 1136(Steve Clark) and last but not least 1138(Adam May on transport, cost and ruggedness).
* Not in the A Class and not known for sure in the Moth class(so far)
=======================
From Tom Speer:
The differences between rigid wingsails and wingmast/sail combinations are mostly in the things you have ruled out.
The slotted flap of a rigid wingsail allows it to achieve a higher sectional lift coefficient than most soft sails. However, soft sails could do better if they could achieve a particular shape, especially if that shape wasn't constrained by having to be a membrane tension structure. The maximum lift has been important in the C-class catamarans, because their area limit makes it hard for them to be fully powered up on the runs.
The control system of a rigid wing allows the wing to be taller without experiencing excessive loads due to leech tension. I believe this was the main advantage of the wing on USA 17 over its soft rig. The control system also makes it possible to control the shape, such as twist and camber, in a more extensive and precise way than for a soft sail. There's no reason why a similar control system couldn't be developed for a soft sail.
There's no reason for the wing to use the same fabric as the soft sail, because the loads are taken by the ribs and spar instead of the fabric itself. Plus, there are two sides to a wing, so that would double the amount of fabric used. If the wing has the same fabric as the sail, it will be much heavier - and far heavier than it needs to be. The wing on USA 17 weighed the same as the mast, boom, mainsail and jib of the soft sail rig. So it was heavier when a headsail was added to the wingsail, but comparable in weight when sailing wing alone.
If the boat is limited by its heeling moment, then the soft sail and rigid wingsail will be trimmed to produce the same lift. USA 17 went to the wing in order to produce that heeling moment in lighter wind.
There's nothing magical about a rigid wingsail. The soft sail rig on USA 17 was faster than the wingsail in some conditions. Whether a wing or soft rig will be faster depends on the class constraints and the sailing conditions.
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