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July 28, 2024 at 8:44 amMudassarbhistySubscriber
Hello,
I’m working on skin buckling analysis for an aircraft wing and fuselage made of composite materials. Could someone provide a step-by-step guide on the following?
- Applying boundary conditions and loads for Wing Skin and Fuselage skin Buckling analysis.
- Selecting and configuring the analysis type.
- Post-processing results to interpret buckling modes and critical loads.
Any detailed tutorials, papers, or resources on composite skin buckling analysis would be greatly appreciated.
Thanks
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July 30, 2024 at 7:05 amAshish KhemkaForum Moderator
Hi,
Please see if the following links help:
Topics in Buckling Analysis | Ansys Innovation Courses
Eigenvalue Buckling and Post-buckling Analysis in ANSYS Mechanical - PADT (padtinc.com)
FLAG simulation – intend to make the fabric drop under gravity (ansys.com)
Regards,
Ashish Khemka
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