Method, based on elastic theory for plate buckling and results for 24S-T aluminum alloy Z-stiffened panels, is shown for calculating compressive strength of Z-stiffened panels that develop local instability.
Method of calculating compressive strength of Z-stiffened panels that develop local instability
Nat Advisory Committee Aeronautics -- Tech Note
1947
15 pages
Report
English
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Compressive Behavior of Frame-Stiffened Composite Panels
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Compressive Behavior of Frame-Stiffened Composite Panels
| NTIS | 2011