Results of tests on 24S-T aluminum alloy panels showed that local buckling strengths increased appreciably with either increase in diameter or decrease in pitch of rivets.
Effect of variation in diameter and pitch of rivets on compressive strength of panels with Z-section stiffeners -- Panels of various stiffener spacings that fail by local buckling
Nat Advisory Committee Aeronautics -- Tech Note
1947
27 pages
Article (Journal)
English
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