TimsCustoms1982 formula is correct, but you need to project the root chord onto the centerline so that fuselage center section is included. Lift from B to D is generated by the fuselage due to endplate effect. That's why the fuselage portion needs to be included in wing area calculations. The blue curve marked "load" shows how lift is distributed over the wing and fuse.
moment%2520diagram.gif
You can also take the wing area of the full scale and divide it by the square of the scale factor. (If the scale fidelity of the model is poor this method may not work.) In my "Cantilever wing spar design" thread, I calculated the Messerschmitt Bf-109 kit #401 wing area to be 97 sq in (= .0627 m^2) but I encourage you to double check my figures.
fw 190.gif
I estimate the wing area of the Fw-190 to be 27887 square inches (dark gray region). The Guillow's Focke-Wulf Fw-190 kit #406 lists the scale as 1:16.
27887/16*16 = 109 sq. in.
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