Investigation being conducted on compressive strength of flat 24S-T aluminum alloy panels for aircraft; tests showed that effect of riveting on strength of panels depended on type of failure.
Effect of variation in diameter and pitch of rivets on compressive strength of panels with Z-section stiffeners -- Panels of various lengths with close stiffener spacing
Nat Advisory Committee Aeronautics -- Tech Note
1947
18 pages
Article (Journal)
English
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