Static structural analysis of cockpit
Description:
Cockpit has composite material: carbon fibre (230GPA) & Epoxy E-Glass UD Thikness 2mm, Element size 5mm Force: front section 1000N downward, fixed support at back
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Attachments:
| File Name | To view or download these files please go to the project page |
|---|
| stress 1.JPG |
| cockpit.wbpj |
| stress 2.JPG |
| stress 5.JPG |
| stress 4.JPG |
| tot def.JPG |