cockpit.wbpj size: 0.065052 MB
stress 2.JPG size: 0.075369 MB
stress 5.JPG size: 0.074745 MB
stress 4.JPG size: 0.076203 MB
tot def.JPG size: 0.078155 MB
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Static structural analysis of cockpit
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About the Static Structural Analysis of Cockpit Project
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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December 10th, 2020 Uploaded
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Aerospace Mechanical Engineering Industrial Design ANSYS Mechanical Structural Analysis FEA Finite Element Analysis Material Engineering Stress Analysis ANSYS ANSYS Workbench
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on December 27th, 2020
on March 10th, 2022