Sorry Cthulhu, but this is incorrect.
P-51D 75% (full wing tanks and a bit in the aux.)
9746lbs/wing area of 235 square feet.=41.5 lbs/square foot.
Dora, full internal, no drop.
9415lbs/wing area of 197 square feet=47.8 lbs/square foot.
(Note that the P-51D can fly farther on just the wing tanks than the Dora can on full internal.)
So there is in fact a very pronounced difference in wing-loading.
BTW, despite this, and the fact that the Dora is equipped with less efficient split flaps instead of maneuvering flaps, DokGonzo's shows the Dora actually maintaining a *smaller* sustained radius with full flaps, wtf? Too bad the flaps won't deploy at a reasonably high airspeed, isn't?
Here's the data I'm familiar with:
Fw-190 D-9 Aerodynamic statistics:Wing-loading *Loaded*: 234.59 kg/sq.m. (48 lbs/sq.ft.)
Wing Aspect-Ratio: 6.02.
Airfoil: NACA 23015.3 - NACA 23009.
Airfoil Thickness Ratio: Root= 15.3% Tip= 9% .
Wing CL-max *Freeflow*: 1.52 .
Lift-loading *Loaded*: 154.33 kg/sq.m. (31.5 lbs/sq.ft.)
Power-loading *Loaded*: 1.91 kg/hp. (4.22 lbs/hp.)
P-51D Mustang Aerodynamic statistics: Wing-Loading *Loaded*: 232.62 kg/sq.m. (47.6 lbs/sq.ft.)
Wing Aspect-Ratio: 5.81 .
Airfoil: "Laminar" NAA/NACA 45-100 - NAA/NACA 45-100.
Airfoil Thickness Ratio: Root= 14.8 or 15% Tip= 12%.
Wing CL-max: 1.28 .
Lift-loading *Loaded*: 181.73 kg/sq.m. (37.18 lbs/sq.ft.)
Power-loading *Loaded*: 2.81 kg/hp. (6.2 lbs/hp.)
As you'd expect, the descrepancy is in the Pony data, the amount of fuel carried is seldom stated clearly, so one has to figure out what *Loaded* means.
Notice the difference in CLmax for both aircraft. Laminar flow airfoils are super slick (provided you keep then spotless), but they're certainly not heavy lifters. They also have attrocious behavior at the limit, something I've never noticed in AH. The conventional wing of the Dora however seems to "cop an attitude" if you even hint at pushing it to the limit.
Anyway, this is a Meteor thread, so we should both probably shut up.