Hi every one,
I am in my final stage of my dissertation, which is about slamming analysis of boat hulls with help of CEL - in Abaqus. I am currently working in how to validate the results which I got. Is there any way except experimental method to validate the stress - strain results?
Please help me...
Regards
Kunal Baxi
M.E.- CAD/CAM
hi, i am Fawad and I am from Pakistan and i am looking for a possible position as post doc researcher in the general area of modeling of manufacturing processes like EDM, Welding. i have exp of modeling welding and Rapid Prototyping process and presently i am working on the development of model for EDM process, i already have 08 journal publication since 2005. My area of research during PhD deals with the thermo-mechanical modeling of welding based Rapid Prototyping with emphasis on reduction of residual stresses and deformations.
hello everyone
i want to model an anisotropic material(hill or barlat) in ABAQUS, in the VUMAT,but I don't know how to set some para such as R0,R45,R90
could you give me a vumat ?
In Féréol et al. (Biophys. J., 2009, 96: 2009-2022),
we propose a coupled theoretical and experimental study in order to understand the
mechanism of cell sensitivity to substrate stiffness. To do so, we first consider
that adhesion sites pass through different stages of development, e.g., Initial
Adhesion (IA), Focal Complex (FC), Focal Adhesions (FA), characterized by the
hi,
Is it necessary to carryout the linear static analysis first before doing the fatigue analysis.
If the stress exceeds the UTS , still can we caryyout the fatigue analysis.
sagar.
Hello everyone, I am studying the dynamic crack initiation problem of composite material. Just like the below imagine ,a crack perpendicular to the interface of two different materials, under dynamic load, the crack will propagate, at the crack tip I use the singular element to simulate the stress and strain state. after I have the crack tip stress, how can I calculate the energy release rate of different direction, for example, also along the original crack line or perpendicular to the original crack line., or kink from the 45 degree of original crack line.
