Hello to all,
I have modeled a assemby (Duct+Brackets) with shell element in abaqus . the FE stress tensor that i found are S11, S22, S33, S12 such as S33=0( Logical for a shell element because these stress value are in element local coordinate system).
Now, I would study the bonding of the...
Thank you jhardy1 for this response :)
what is the buckling factor for internal section loading? it is a analytical value or given by a tabular data ?!!!
can you explain me more ?
Hello
in same scenario, I have onther question: the Buckling load factor is it the eingenvalue given by abaqus for each mode ??!!
Please, i wait your response!!!
Hello to all,
i'm biginner in FEA Composite by abaqus software.
i have done a buckling analysis with 10 modes for a Composite component under pressure 0.001 MPa.
As results,(1) the eingenvalue for 1st buckling mode (as exemple) is equal to -0.0523. if it's correct as result, why it's negative...
