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Static Analysis
Fatigue & Damage Tolerance
Finite Element Analysis
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STRAND Malaysia
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Airbus A380
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Linear Analysis
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STRAND has performed linear analysis using PATRAN/NASTRAN for both wing structure and landing gear.  Previous work has involved modelling, validation (including test correlation) and post-processing.

 

Search the links below for details of some of STRAND's projects. 

Computer Racks
Landing Gear
Wing Structure