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Paducah said..
but realized that I was looking at the wrong frame of reference. It's the board that actually rotates, not the fuselage. The wing operates under a pretty restricted angle of attack.
Yes and no.
The fuselage isn't a completly fixed reference. Only at a constant speed with a specific weightload (rider & equipement). For those that can claim different cruizing speed depending on condition (ie top racers), the fuselage angle can change significantly. From my guess, AOA range can be from 1 or 2 up to up to something like 12? up (my rough guess of what is the stall angle of the foil, but of course only designer can give you the exact value of stall angle, wich by the way is a fixed value whatever the speed).
So indeed if you draw the figure, the mast tilt forward by the same angle when you accelerate. At very low speed it can be quite nose up and the weight is moving back, and that makes recovery from this attitude can be tricky.
But shimming usually change by a couple of degrees the board pitch, and the goal is more to manage higher speed. Low speed (when you get behind the best glide AOA bump) is so clumsy you should always try to pass forward. I don't know the english vocabulary for this effect (in french 'second r?gime') but at a certain AOA profile drag start to increase thus you need more trust force to maintain flight when speed decrease (AOA increases) whereas when you get ahead, drag decreases when speed increases (AOA decreases). Up to a ceratin point of course when drag from speed becomes the major factor.