I also like the reed-style horns.
I believe locating it at the location of the stagnation point as determined by tuft testing would be wrong by an inch or so. The stagnation point is a high pressure area (just like the front of a pitot tube). That is where you would install the switch style sensor.
The point you really want is one that becomes low pressure relative to the cabin and is probably an inch or two ahead of the stagnation point. Probably close to but slightly below the leading edge.
Here's a video that shows the relation between pressure and flow streamlines.
https://www.youtube.com/watch?v=edZLT9eymIkYou could probably get close by copying the placement from another airplane, but the Sonex is different enough that I'm not sure you could do it without needing to adjust the placement slightly.