retroaviation wrote:
You can see the paint lines on the cowling displaced, along with the wrinkles in the fuselage.........
Wrinkles on the bottom side of the fuselage, if on both sides, would indicate that the skins are under a compression load. In a steep turn (high positive "G" loading) the tail is pushing down very hard to keep the nose up, indeed putting the lower portion of the fuselage in compression. The horizontal stabilizer is counteracting the forward pitching moment of the wing airfoil. The upper fuselage skin, in tension, gets stretched tight so you don't see any deformation.
I have been in formation next to a polished T-28 and seen the talicone wrinkle back and forth as we bounced around in turbulence. That is normal though as no airplane is infinitely stiff. If you look at a B-52, you can see wrinkles in the fuselage and that is when it is sitting on the ground stationary.
I do not doubt the story about damage in the tail in the least, I only suggest the cause was most likely not torque. This aircraft has seen a lot of time in steep turns at high speeds in gusty and turbulent conditions, so highly stressed areas could suffer from fatigue damage and crack. This aircraft also suffered an accident at one time (cartwheeled as I recall in the early 60s) so there may have been some unseen damage from that incident that may have contributed to the condition discovered.
The displacement of the paint lines is clearly due to torque (unless they installed the cowling crooked!). I'm only semi-knowledgeable in aerodynamics, but I would expect that the engine torque is mostly reacted by the ailerons with a little help from fin offset (which is probably set for cruise speed). At the speeds seen in Reno it doesn't take much aileron displacement at all to counteract the torque.