drgondog
Major
The changes to the inner structure of the wing when moving from NA-83/91 wing to A-36 were not major issue, structurally speaking because the dominant loading remained Angle of Attack load for high G turn and dive pullout.
The dive brake introduced new load considerations but the stresses to internal wing structure like the spar and external structure such as skin thickness to increase torque box rigidity were only to increase 0.040 to 0.64 along the leading edge.
The dominant load factors were drag and sideways loads which introduced moments to the new bomb rack plus introduced aerodyamic safe load envelope to approximately 400 mph on the dive brakes. The latter mandated a warning in the operating manual of the A-36 to ALWAYS open dive brakes BEFORE exceeding 350mph and before entering a dive. There were two fatal A-36 accidents when two French pilots entered their dives before the brakes were extended. Both had catastrophic failures at WS 75 - which led Training Command to order the brakes wired shut and limit bomb load to 500 ponds). The A-36 was analyzed and accepted for 1000-pound (each) bomb loads.
The centroid of the rack was at ~ 33% chord, the location of the main spar. IIRC the A-36 only had the B-7 bomb rack which was rated at 1,100 pounds. That said the P-51A/B pylons were stressed for 600 pounds and that the D did not introduce any internal structure for the D when the new pylon and B-10 equivalent rack was installed for 165-gal external fuel tanks.
All leading edge skins for A/B/D continued the A-36 leading edge skin dimension of 0.064.
The comments above regarding the design opportunity to introduce both controls and conduit/wire bundles for controlling both the bomb and the drop tank are correct.
The primary difference in design philosophy favoring P-51 and P-38 over the P-47 was that both were focused on wing tankage (and structure) from the beginning design, and both were designed for 150/330-gal wing tanks in 1942. When Republic was being hounded by Materiel Cmd to add wing pylons to carry droppable 150+gal tanks, thy had to modify many P-47C/D in the field - which was a depot level modification to open up the wing forward of the spar and add both fuel lines and controls. I have never seen the structural analysis for the P-47 as all were destroyed by Fairchild when they acquired Republic.
The dive brake introduced new load considerations but the stresses to internal wing structure like the spar and external structure such as skin thickness to increase torque box rigidity were only to increase 0.040 to 0.64 along the leading edge.
The dominant load factors were drag and sideways loads which introduced moments to the new bomb rack plus introduced aerodyamic safe load envelope to approximately 400 mph on the dive brakes. The latter mandated a warning in the operating manual of the A-36 to ALWAYS open dive brakes BEFORE exceeding 350mph and before entering a dive. There were two fatal A-36 accidents when two French pilots entered their dives before the brakes were extended. Both had catastrophic failures at WS 75 - which led Training Command to order the brakes wired shut and limit bomb load to 500 ponds). The A-36 was analyzed and accepted for 1000-pound (each) bomb loads.
The centroid of the rack was at ~ 33% chord, the location of the main spar. IIRC the A-36 only had the B-7 bomb rack which was rated at 1,100 pounds. That said the P-51A/B pylons were stressed for 600 pounds and that the D did not introduce any internal structure for the D when the new pylon and B-10 equivalent rack was installed for 165-gal external fuel tanks.
All leading edge skins for A/B/D continued the A-36 leading edge skin dimension of 0.064.
The comments above regarding the design opportunity to introduce both controls and conduit/wire bundles for controlling both the bomb and the drop tank are correct.
The primary difference in design philosophy favoring P-51 and P-38 over the P-47 was that both were focused on wing tankage (and structure) from the beginning design, and both were designed for 150/330-gal wing tanks in 1942. When Republic was being hounded by Materiel Cmd to add wing pylons to carry droppable 150+gal tanks, thy had to modify many P-47C/D in the field - which was a depot level modification to open up the wing forward of the spar and add both fuel lines and controls. I have never seen the structural analysis for the P-47 as all were destroyed by Fairchild when they acquired Republic.
Corrected my post up-thread.