Randy Haskin wrote:
Do any WIXers have photos showing over-stress damage to aircraft? More specifically, I need a shot showing either popped or pulled-through rivets.
Don't have a photo handy, but rivets that are overstressed will either shear (the shank will be cut through by the sheets of skin), pull through after curling up the edges of the rivet heads, or pull the rivet head off. An incipient rivet pull through would show the edges of the rivet curled up so that there is a depression in them (on a flush head rivet). Sometimes the countersink in the skin looks virtually undamaged. Protruding head rivets normally don't pull through. Rivets usually pull through from skin buckling which imparts a normal force on the rivet head. Current design practice dictates that the skin should fail before the rivets pop though. After all, if the fastener fails there is more strength capability left in the remaining structure that is not utilized.
Crash damage is a good place to find what you are looking for since the forces imparted follow load paths that were never intended by the designer.