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
Embed Code for Static Structural Analysis of Cockpit
Copy the embed code below to include this project on your website:
Static structural analysis of cockpit
NoAI: This project, including models, simulations, images, and descriptions, may not be used within datasets, during the developmental process, or as inputs for generative AI tools.
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
Statistics
12 Downloads
2 Likes
3282 Views
2 Comments
6 Files
0 MB Project Size
December 10th, 2020 Uploaded
Share
Share Tweet Pin Share Share Post ShareTags
Categories
Aerospace Mechanical Engineering Industrial Design ANSYS Mechanical Structural Analysis FEA Finite Element Analysis Material Engineering Stress Analysis ANSYS ANSYS Workbench
Sponsored Ad from FindingDIY
Related Projects
Sign up to join the conversation about Static Structural Analysis of Cockpit
Post a comment! Share insights on Static Structural Analysis of Cockpit , ask questions, and connect with other users. Whether you're curious about the 3D model, fluid simulation, or finite element analysis, your comments enrich the conversation.
on December 27th, 2020
on March 10th, 2022