Basic assumptions of conventional riveted joint design practice are discussed with respect to their applicability to aluminum alloys; data presented to establish effect of holes on tension efficiency of 24ST aluminum alloy sheet, and values are proposed for use in riveted joint design. Before Inst Aeronautical Sciences.
Tension joints in aircraft structures
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 10 , n 8
1943
Article (Journal)
English
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