hrtuwair
Civil/Environmental
- Jun 15, 2013
- 14
Hello all,
I am modeling a sandwich composite beam in ABAQUS. The material I am using is linear elastic up to failure. I defined E and v in the material properties but don't know where should I define the ultimate stress and strain (i.e. failure stress and strain). I tried to define them in the plastic model but the resulted force-deflection was nearly linear-perfectly plastic, which was not similar to the experimental result. The experimental result curve of the force-displacement at mid-span was almost linear up to failure which was caused by crushing under the loading point.
Any suggestion please in how to model the ultimate stress and strain of a linear material in ABAQUS?
Your help is appreciated.
Thanks
I am modeling a sandwich composite beam in ABAQUS. The material I am using is linear elastic up to failure. I defined E and v in the material properties but don't know where should I define the ultimate stress and strain (i.e. failure stress and strain). I tried to define them in the plastic model but the resulted force-deflection was nearly linear-perfectly plastic, which was not similar to the experimental result. The experimental result curve of the force-displacement at mid-span was almost linear up to failure which was caused by crushing under the loading point.
Any suggestion please in how to model the ultimate stress and strain of a linear material in ABAQUS?
Your help is appreciated.
Thanks