Compression tests on five stiffened N8 aluminium alloy plates covering typical full scale warship scantlings are described. The panels were manufactured using normal shipyard production methods to ensure typical initial distortion and residual stresses. Maximum loads and post-buckling load/deflection results are compared with theoretical predictions using the ARE computer program N106C. Keywords: Buckling, Strength, Test, Compression, Stiffened plate, Interframe, Yield.
Interframe Buckling of Aluminum Alloy Stiffened Plating
1985
68 pages
Report
No indication
English
Nonferrous Metals & Alloys , Marine Engineering , Aluminum alloys , Metal plates , Steel , Buckling , Compression , Deflection , Distortion , Loads(Forces) , Naval vessels(Combatant) , Predictions , Residual stress , Test methods , Theory , Stiffening , Panels , Frames , Structural engineering , Foreign technology
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