I have some thoughts and ideas on foiler design that I would like to throw into the mix for your attention. As I am still catching up with this thread, and have only reached the halfway point, pardon me if I mention something already covered.
- a number of issues have been discussed but control of height and pitch (CHAP) still seems to be open to discussion and perhaps improvement. While gifted individuals are able to balance a fast-moving sailboat and manage the rig while simultaneously planning race strategy, adapting tactics to the demands of the moment, keeping an eye on wave and wind conditions together with their competitors and handling CHAP, perhaps this is not for everyone. It is certainly not for the People’s Foiler mentioned once or twice.
There is literally an extra dimension involved in foiling than in sailing a dinghy, which can be complicated enough, and I for one, although not (yet) a foiler, can appreciate the desire of some to automate some at least of the flight control issues on boats with fully immersed foils.
Aircraft design practice has been quoted as a source of theory for foiler design. Foilers can certainly learn from aircraft design but the design of airfoil- and hydrofoil-supported craft is not exactly parallel. Here are some examples of differences:
1) Aircraft wings do not operate just below a medium discontinuity (the surface) like boat foils.
2) Boat foils do not have to operate during takeoff and landing just above a medium discontinuity (the ground) like aircraft wings.
3) An aircraft can lose far more height than a foiler without coming to grief.
4) A (foiled) sailor has a better chance of surviving a crash.
-so the same design guidelines may not apply to both aircraft and foiling boats.
It has been stated that for static flight stability the center of gravity must be in front of the neutral lift point, which is the center of area of combined main wing and stabilizer. This is true for aircraft, canard or conventional, where the rear flight surface must operate at a lower angle of incidence (alpha) than the front. This ensures the front surface is closer to stalling; then if the nose rises and alpha increases forward lift is reduced and the nose drops. Although the rule has been ignored in some aircraft that actually flew in for distant years, few if any of those aircraft survive.
If manual CHAP is intended the rule should probably be obeyed; probably but not certainly, because the theory of foiler flight is not yet mature. However, the rule is ignored in aircraft using fly-by-wire, and a foiling boat that uses feedback from a surface sensor for CHAP has the equivalent of fly-by-wire.
Ideally, automated CHAP should achieve level flight ensuring the foils remain immersed and the hull does not get wet. Wave following and porpoising are undesirable as either can lead to a crash and will drain off forward momentum.
I believe a boat using immersed foils should have a single lifting foil and a single control foil, much like an aircraft. This does not exclude multi-plane designs where several lifting foils are stacked vertically, if it has an advantage. The boat should ideally be balanced on the lifting foil and the control foil should be only large enough to react necessary movement of crew. In a boat perfectly balanced over the lifting foil the movements of the control foil can be very slight, letting the inertia of the boat average out pitch fluctuations and requiring only long-term, slow response control over the average height.
However, this concept does not accommodate the bow-down moment from the rig. Some changes are required for this and several solutions come to mind.
A lifting rig can be used to eliminate the bow-down moment from rig thrust: a mast-aft rig or lateen sail can do this. A separate lifting airfoil can be deployed when foiling -this could even be a small flying jib. I have seen pictures of foilers with gennakers elsewhere in the forum that clearly can provide considerable lift. Or the CoG could be moved aft of the lifting foil, enough to offset part of the rig’s bow-down moment and the control foil enlarged to accommodate the rest. I personally am inclined towards solving the problem of bow-down moment in the air since any such arrangement would also handle gusts.
A foiler must transition from displacement (or planing) mode to flying mode.
In displacement mode it is probably easier to raise the bow than to lower the stern for takeoff. The CoG is generally closer to the stern than the bow when sailing so it makes sense to me to use a forward location for the control foil.
However, a small control foil will not have the power to raise the bow enough for slow-speed takeoff. Here I believe we can learn from aircraft practice, which is to use flaps. The flap need not be nearly as large as those used on aircraft, where the flaps are fully extended for landing where the extra drag steepens the glide slope but only partly extended for takeoff to minimize drag.
I am reminded of a method I once used to automate “liftoff” of a highspeed catapult-launched model glider. It had a delta wing with an elevator that was forced down by air pressure at the high takeoff speed for a smooth climb-out and raised at height by a rubber band to transition into a glide after losing speed. It worked extremely well but was banned due to its takeoff speed estimated in excess of 80 mph; the catapult was about 150 ft (50 m) long! The same principle should work with a flap on the lifting foil to increase lift at low speed for takeoff and reduce drag at high speed, except the flap would be lowered for low speed operation. It might also help to provide a softer “landing” by increasing foil lift again as speed is reduced.
Although manual control of main foil lift by a lever would work, the automated system above would actually be simpler and more compact.
Once flying, if automated CHAP is used it should be effective but with a minimum of added drag. I am not sure at this point whether the control foil should have a flap or be pivoted. Whichever turns out to be optimum, the sensor and feedback system is critical to success.
Most of the successful systems to date seem to use a surface sensing wand with a mechanical linkage. Other than surface piercing foils, there does not seem to be many alternatives in use. I will try to think out of the box and throw out some ideas.
If the forces required for pitch control can be kept small enough, it may be possible to use the variable buoyancy of a tapered strut for fine pitch control, using the control foil for manual, coarse corrections.
Another depth sensing arrangement not yet tried as far as I know uses hydrostatic pressure feedback. In one method, a lightly-loaded hollow foil is designed to vary its lift by changing profile in response to variations of pressure. Alternatively and easier to design, a streamlined bulb made of flexible material is mounted on a rigid wand behind a forward-mounted pivoting foil; if depth increases it compresses and loses buoyancy, so it falls and increases the alpha of the control foil, raising the bow. A rigid bulb with a small hole would do the same and adjusting the hole size would provide variable damping; an internal bladder would prevent expulsion of air if necessary. These concepts are all robust, self-contained, simple, low drag and weed-free, with no linkages to worry about.
The above ideas for controlling pitch are also applicable to automatic heel control, of course.