My understanding was that the main benefits from a delta wing planform came when operating at high subsonic, transonic, and supersonic speeds.
There is some re-energisation of the boundry layer due to the tip vortex rolling over the top of the wing, which gives them a very high stall angle. This is useful on high speed aircraft as they need to operate at a high angle of attack at low speed as the wing area needs to be small to allow for high speed flight. The good stall caricteristics may be why they are used on the foiling kites.
It is worth looking at the performance of a for a few foils shapes to understand the range of angles of attack that are worthwhile. If you look at the drag polar for the H105
here you can see that there is a big increase in drag when the coefficient of lift is around 0.8, this corresponds to about 5 degrees. the foil still seems to be generating lift up to about 10 degrees, so the drag increase is happening well before stall.
The optimum foil size is going to depend on the all up weight, how much the hull drag drops with a reduction in displacement, and how the foil drag increases as you increase the lift. Match this with the expected wind conditions and you will know how big to go. Alternatively just go two boat testing.