And this puts their wingloadings at 6.46lbs/sqft for the Dr.I and 6.30lbs/sqft for the Camel.
Wingloadings with full fuel:
Dr.I: 6.46lbs/sqft
Camel: 6.30lbs/sqft
This is why wingloading figures alone shouldn't used when comparing maneuverability:
A pic depicting the Göttingen 298 used in the Dr.I:

The airfoil used in the Camel, third from the top:

Dr.I uses overall much more efficient airfoil which creates more lift in relation to its drag. One thing of course is the interference between wings of the Dr.I and how much it negates this advantage but it doesn't surprise me that Dr.I has a smaller turning radius.