Here's a link to one of Steve's articles. http://www.plucks329s.org/pdf/frame/Evolution_of_the_frame_assembly2.pdf
Bob
Bob
I know you all are getting tired of my posts but here is one more question. In the aircraft industry all rivets are bucked with a flat bucking bar to get the desired 1 1/2 diameter and 1/2 diameter tall tail. I know this isn't a 747 but why all the procedures to produce a different tail shape? Is is to try and replicate Fords rivets or is there a stuctural reason for this steel application? Also, what degree is the front crossmember frame counter sink and if hammered from the top is the top or bottom of the countersink hole used for unbucked rivet length?
John