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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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12 Downloads
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2 Comments
6 Files
0 MB Project Size
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