P52 Progress as of March 2015

Work on P52 has progressed slowly over the Washington winter.  Both bunks and both foredecks were removed as they had deteriorated beyond repair.  New ones have been made but not installed yet.  All of the interior has been sanded and epoxy coated where needed.

I have been concentrating on the wing design and that is now finalised.  Control of the wing and tail has been a challenge, but I have finally built a de-coupler that will set the angle of attack of the wing independently of the orientation of the hull.

The ama and half of the vaka have been sanded and painted with Glidden's white primer and sealer.  I will use their Porch and Floor polyurethane oil paint for a top coat when the weather improves enough - I have to work outside!

Some pictures:

Starboard bow with the old deck removed

Removal of the bunks leaving a ledge for the new bunk to sit on

Port bow with the deck removed

De-coupler pieces awaiting assembly

Bunk area cleaned up and epoxy coated - note mast support lower hole at far end

Upper support for mast support tube

Mast support tube in place - yet to be epoxied in

Interior view - Mast support tube in place - one at each end

Aluminium wing tubes in the mast support tubes.

6061 T6 3 inch OD 1/8th wall thickness, 8ft long.

View of stbd wing tube

View of port wing tube with de-coupler fitted.

It will be clearer how it works once I have built the wings.

De-coupler on the aluminium wing tube.  

The top part that I am holding is glued to the lowest wing rib so is at a fixed height but will rotate with the wing.  It forces the upper part of the lower assembly to rotate with it.

The lower assembly can move up and down on the wing tube but only the top piece of it can rotate with the wing.  The rest of it is to be attached to the mechanism that moves it up and down so as to actuate the bell crank in the wing that will alter the angle of the tail and the flap.

We will be moving to Florida during April and will be camping in a site near St Augustine.  We have booked a site on the west coast of FL so as to be able to attend the messabout at Cedar Key during the first weekend of May.   See you there!

Current status as of Nov 11th 2014

Here is a picture of the P52 proa built by Skip as she is now outside my house in Coupeville, WA.  She will be renamed, fixed (decks, sides, cockpit, etc.)  The bow decks will be modified to hold the two wingsails that will be free-standing.  Then a cleanup and paint - yellow of course!  Lots of work ahead.

Proa P52

 Skip's proa with wing shown at the SailOK mess-about at Lake Eufala in 2014.  Skip made me aware of the work done by Dr. Elkaim.

Skip's Proa 

Details of the control system on Skip's proa at SailOK 2014.

Wing control details

Dr. Gabriel Elkaim's dissertation

I need to give credit to Dr. Elkaim for his work on wing sails in a low Reynold's number environment.

His dissertation is titled, "System Identification for Precision Control of a Wingsailed GPS-guided catamaran", and was published in December 2001 at Stanford University in partial fulfillment of the requirements for the Degree of Doctor of Philosophy.

I found this paper to be of great help in my deliberations on the design of a wingsail system for use in a proa sailboat.  Specifically the wing design and layout, with some modifications, are what I will be using on the proa.

There will be two wing systems, one on each bow.  The control system, however, will be entirely mechanical so that the wings may be controlled by the skipper of the boat.  As there are fundamental differences in the way a proa is sailed and the way a catamaran is sailed (shunting vs. tacking or gybing), the wings will be used with a different control system than the one designed and built by Dr. Elkaim.  I will be detailing this control system once I have built it and worked out the bugs.

Thoughts on the wings

Some proagress has been made on the wing design.  Dr. Elkaim’s dissertation cites some problems with the NACA 15% section at low Reynold’s numbers as there is a separation bubble formed just aft of the nose on the leeward side of the airfoil.  

As a result he finally decides on a 21% section with a zig-zag trip strip at 22% of the chord to promote turbulent flow aft of the trip strip.  I have decided to go a little simpler by using an elliptical section at the front of the foil to avoid the small nose radius of the NACA sections.  Otherwise the section is as specified by Dr. Elkaim, except it is fractionally smaller.  It is easy to make an ellipse and if it does not work, it is not terribly hard to change the nose section of the wing.

The wing will be based on standard 4x8 sheets, so will have a chord of 4ft and a span of 16ft.

The wing will be constructed as follows:

1. Build the spar and web as a complete unit using 3mm ply for the web and a 16ft length of spruce (left over from mast building) for the spars.  The width of the web is 10 inches and the spar will be made in two parts glued to either side of the web edges (4 lengths in total).  The web at the base of the wing will be thickened to 6mm by either doubling up on the 3mm ply or using 6mm ply.
2. The wing pivot is to be at the quarter chord position.  As the spar/web assembly is at the 21% chord, the wing pivot will be made from a 3.5 inch aluminium tube glued and fixed to the rear of the spar/web assembly.  This will fit and pivot inside a 4 inch aluminium tube glued and fixed into the two foredecks of the proa.  Thus there will be two wings, one at either end of the main hull.  They will be free to rotate about 360 degrees and their angle of incidence will be controlled by the angle of the tail.  There will be a flap at the trailing edge of the wing.  It will have a chord of 13% of the wing chord.  It will be deployed in the opposite direction of the tail.
3. The nose of the wing will be formed by gluing thin bending ply over plywood formers that have been glued to the front of the spar/web assembly.  The bending ply will extend over the spar and will form the start of the aft part of the wing.
4. The tail section will be built the same way.  This shows the layout of the two and their spacing.
5. The control system will de-couple the wing from the hull so as to allow the wing to maintain the same angle of attack regardless of the orientation of the proa hulls.  Dr. Elkaim found that if the wing angle of attack was reversed too early in a tack it would stop his catamaran and start it going backwards.  This is exactly what we want in a proa as it does neither tack nor gybe.  Thus, reversing the angle of attack of the wings will almost automatically bring about a shunt.  We will see what happens in practice.

Once I am back in Washington I will post some more details of the hulls when I get them off the trailer.

The platform is here

I picked up proaskip's 24ft proa hulls from Kevin O'Neill on our way through Texas to the Port Aransas Wooden Boat Festival.  We are on our way back to Washington.  I have read, marked and learned Gabriel Elkaim's dissertation published in 2001 on his wing sailed catamaran.  Good stuff.  Now I am designing the wing(s) that will go onto the hull of P52 - to be renamed.  Once I get back to Coupeville, I will take some photos and post some more stuff.

Thanks Skip and Kevin for making this possible.