I don't get these buckling load ( 209 !!!!).
and I habe been playing with all BC possible.
and including 3D solid model.
I tried to do it and I don't get the same, could you let me know what are the frequency of your model ( just for me to verify) and what is the stress for your static...
Thanks rb1957
To be more clear:
1) Load is: newtons per unit length ( N/mm)..not pressure (let try not confuse with my original case post..let run the simple case as described before).
2) Before to run a skin model for load distribution, let set the model for as simple ring as described before...
Thanks all.
Sorry if I mix up some numbers.
Let fix the case for future reference to R= 1000 mm .
Square section: 25x25 mm
I: 32552 mm4
Yes, material is steel E=193053 N/mm
Load case: unitary external force 1 N/mm (since my benchmark model is beam element)
Timoshenko buckling pressure: 18.85...
Does any body know the equation for the buckling modes for a solid ring under external pressure.
inplane and outplane modes?
related forum:
http://www.eng-tips.com/viewthread.cfm?qid=287836&page=1
Hello John
I am trying to model a fuselage section, basically simple assumed as a one support ring and a cylindrical shell skin under external pressure. (like a submarine)….
I want to see the stress in the ring, as you could image, the ring is free in the space but supported by the shell skin...
CORUS: Well, the only way for a model to run without constrains is for modal analysis only, so I will agreed that the first 6 modes will give you the 6 rigid movements, but for a Buckling analysis with not constrains I don’t see how to do it (and I will guest is not possible).
I am looking to...
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Hello, Pio3 and Petiesmo.
I got two different points regarding with the FEA analysis that Pio3 is doing.
Regarding with the fea analysis in plastic like material, please have a look at the thread “ Pro/mechanica and plastic like materials”, so we don’t mix opinion in this thread.
Now...
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