"When arranged in a true monocoque structure or a single spanwise spar and skin then it's simply a question of a higher tolerance to localized damage over a very broadly distributed stress system."
All the monocoque structures have a problem with projectiles of chemical composition since these are made to rapidly increase pressure inside the structure and rip it apart, that is, the main supporting structure. Because the thickness of the surface was greater I still don't think where was not a millimeter (that is 0.03937008 inches) of excess thickness due to creeping weight which plaqued the wooden aircraft structures. What was better with aluminum was that the metal would in some cases give in and bulge under pressure, where as the wooden structure would simply shatter due to its nature of being a natural composite of fibrous cellulose suspended in a lignin matrix+glue.
What was better in using wood was the nonstrategic nature of the raw material, uniform surface of the resulting skinning and, I'd bet, the resiliency to "tiring" which was a problem with aluminum designs, which after a time contributed to speed loss and sloppy maneuverability due to slowly increasing leaks and structureal elasticity. But laminated wooden structure is slow to manufacture and hard to make last in rough field conditions, as the Russians found out, and Brits, of course, when the upper surfaces of the wings began to depart the Mossie airframes.
"No magic necessary. Unless you're talking about the designers of course."
Not really. The solution was not magical, nor the designer were capable of that, not even if many people would like to believe that.
If it was, our planes today would be built of wood instead of steel, aluminum and advanced composite materials.
-C+