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IL-2M3 Wing Loading
WW2 Warbirds: the Ilyushin Il-2 Shturmovik - Frans Bonn
Up to 2,205lb bomb load.
Wing loading: 34 lb/ sq ft @ maximum weight.
Ju-87D1 Wing Loading
WW2 Warbirds: the Junkers Ju 87 Stuka - Frans Bonn
Up to 3,968lbs bomb load.
Wing loading: 42 lb/ sq ft @ maximum weight.
P47D-22 Wing Loading
WW2 Warbirds: the Republic P-47 Thunderbolt - Frans Bonn
Wing loading: 54 lb/sq ft @ maximum weight.
How accurate was P-47 weapons delivery, with a wing loading that high?
The Bristol Blenheim and Fairey Battle had the potential to bomb accurately. But bombing tactics, aircrew training and enemy opposition still matter.Considering the last two it is a wonder the Germans managed to get across the Bridges at Sedan.
A study on of fighter-bomber attacks on bridges over the Savio River in Italy during the spring of 1944 found a sharp drop-off in bombing accuracy directly correlated with the intensity of flak fire. With no flak, P-47s could put half of their bombs within 180 feet of their target and required 30 bombs to score one hit. With medium flak, accuracy dropped to 300 feet, requiring 84 bombs per hit; with heavy flak, it was 420 feet and 164 bombs.
JU-87 Stuka, Hawker Typhoon, P-47 Fighter bombers
If this is correct then we have data for comparison of bombing accuracy.
Accuracy with no flak.
P-47. 30 bombs required to score a hit. 50% within 180 feet of target (360 foot circle).
Ju-87B. 25% success in hitting the target for average pilots.
Ju-88A. 50% of bomb load within a 50 meter circle.
If I were a soldier desperately in need of CAS the P-47 would not be my first choice. Better to place 500lbs on target then to miss with 2,500lbs (or place it accidently on friendly units).
I suspect the A-36 dive bomber was better at putting steel on ground targets then the better known F4U and P-47 fighter-bombers. But for some reason the U.S. Army Air Corps chose not to continue development. They could have added survivability enhancements like dual radiators with individual cut off valves (similiar to Me-109) and additional cockpit armor. Increased aircraft weight would be offset by more powerful versions of the Allison V-1710 engine. Poor performance at high altitude (for the Allison engine) would not be an issue as this is a CAS aircraft.