While the temps on our Aerovee are a lot better, and a whole lot more even across cylinders, than they were before we installed the custom plenum, we are still unable to climb for more than ~80s at Vy before the CHTs hit 400+F, and we can't really climb at less than maybe 110mph without eventually getting above that temperature. This might improve as the cylinders get more broken in, but one topic that I've been wondering about since getting the Sonex is the apparently-suboptimal inlet shapes in the cowling.
Basic aerodynamic principles say that inlets should have rounded lips and then a fairly gradual diverging shape on the inside. The Sonex cowl violates both of these principles for both the cylinder and oil cooler inlets. At least on our airplane, the openings have sharp edges without the slightest amount of rounding. I suspect the airflow into the inlets could be improved by giving them a rounded edge and an internal diffuser. The way the cowl fits, this is not straightforward, though. I was wondering if anyone's already experimented with altering the shapes of the inlets.
Although now I'm looking at pictures on the Sonex web site, like
that appears to have rounded edges. Maybe the openings on our cowl were cut too large? Or has the design been changed? I don't have a picture of it handy. The oil cooler inlet seems to still have a sharp edge though.