Rick Loheed
Junior Member
- Joined
- Mar 16, 2006
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- Maryland, USA
Mast Rotation
I'll probably get in trouble here- aside from the fact that every case is a different problem in general, the fact that a sloop rig comes into it's own on heavier boats- whereas a single wing or well done cat rig works better for high speed- is no surprise to me. The game for lightweight high speed boats is more one of striving for max L/D simulteneously with max CL, whereas heavier boats tend to need Max CL. Speeds are lower, boat drag is higher, it's not as 'knife edged' of a design problem. Since the jib/main combination is widely adjustable, and high lift, it can sort of do both and you can usually change the headsail size.
For a nice wingmast discussion, and more on the aerodynamics of these things visit http://www.tspeer.com/ if you haven't already.
I don't have recent experience with the boats you mention, I sail a C&C 24, my sailing canoe, and an E-Scow, none have rotating masts but the sailing canoe sail is pocketed. The E-Scow of course is plenty fast.
However, I have had experience with rotating (but not wing) masts, both on an M-16 Scow as well as on small Catamarans. Overrotating allows the mast to bend more forward, tending to flatten the sail shape considerably in heavy air. Typically though, the M-16 carries more camber cut into the main sail (meaning there is more to remove) than a cat. Can these wingmast rigs bend laterally?
Here is a comparison using Javafoil of a simple 15% camber (pretty high lift) 40% max camber location Jib/main combination arbitrarily loaded to near Max CL, and a 20% Clark 'Y' wingmast shape based on methods from Tom Speer's wingmast paper. For an input Aspect ratio of 10 for each case, this simulation shows a Max Cl of 2.11 for the main jib combo readily achieved for the combination, whereas the wingmast gets to a fairly typical Cl of 1.2 max. before separation occurs. I did not look at the polars, I have to get to work- but the point here was about max CL. I need to read Martin Hepperle's web site to find out how he's implemented the aspect ratio corrections in a 2D section study, but for now I will assume it analyzes the center-span pressure distribution for a rectangular planform. It's the only quick multi-element 2D foil simulator I have...the VLM code would take longer and this has to happen over coffee this morning...
it should be a pretty fair apples to apples comparison and it's meant for illustration only.
I'll probably get in trouble here- aside from the fact that every case is a different problem in general, the fact that a sloop rig comes into it's own on heavier boats- whereas a single wing or well done cat rig works better for high speed- is no surprise to me. The game for lightweight high speed boats is more one of striving for max L/D simulteneously with max CL, whereas heavier boats tend to need Max CL. Speeds are lower, boat drag is higher, it's not as 'knife edged' of a design problem. Since the jib/main combination is widely adjustable, and high lift, it can sort of do both and you can usually change the headsail size.
For a nice wingmast discussion, and more on the aerodynamics of these things visit http://www.tspeer.com/ if you haven't already.
I don't have recent experience with the boats you mention, I sail a C&C 24, my sailing canoe, and an E-Scow, none have rotating masts but the sailing canoe sail is pocketed. The E-Scow of course is plenty fast.
However, I have had experience with rotating (but not wing) masts, both on an M-16 Scow as well as on small Catamarans. Overrotating allows the mast to bend more forward, tending to flatten the sail shape considerably in heavy air. Typically though, the M-16 carries more camber cut into the main sail (meaning there is more to remove) than a cat. Can these wingmast rigs bend laterally?
Here is a comparison using Javafoil of a simple 15% camber (pretty high lift) 40% max camber location Jib/main combination arbitrarily loaded to near Max CL, and a 20% Clark 'Y' wingmast shape based on methods from Tom Speer's wingmast paper. For an input Aspect ratio of 10 for each case, this simulation shows a Max Cl of 2.11 for the main jib combo readily achieved for the combination, whereas the wingmast gets to a fairly typical Cl of 1.2 max. before separation occurs. I did not look at the polars, I have to get to work- but the point here was about max CL. I need to read Martin Hepperle's web site to find out how he's implemented the aspect ratio corrections in a 2D section study, but for now I will assume it analyzes the center-span pressure distribution for a rectangular planform. It's the only quick multi-element 2D foil simulator I have...the VLM code would take longer and this has to happen over coffee this morning...
it should be a pretty fair apples to apples comparison and it's meant for illustration only.