- #1
Rawllet
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- TL;DR Summary
- Tensile test, using ACP Pre and Static Structural modules, of a fiber glass laminate with 6 layers orientated +/-45°.
Hello everyone!
I am trying to modelate a tensile test of dumbbell-shaped specimen under ACP PrePost and Static Structural modules. The laminate I am configuring consists of 6 laminas of E FiberGlass orientated +/-45°. For simplicity I am working with 1/4 of the geometry and the boundary conditions are 2 displacements. One that let's movement only in X axis and the other only let's movement in Y and Z axis.
My problem is a strange deflection that is shown in the solutions spot and I do not know what could be the reason of it. I don't know if is because of the boundary conditions or maybe a bad laminate configuration.
I wii be very thankful for any help. I attached a few photos that could help in the understanding of the problem.
Thank you in advance.
I am trying to modelate a tensile test of dumbbell-shaped specimen under ACP PrePost and Static Structural modules. The laminate I am configuring consists of 6 laminas of E FiberGlass orientated +/-45°. For simplicity I am working with 1/4 of the geometry and the boundary conditions are 2 displacements. One that let's movement only in X axis and the other only let's movement in Y and Z axis.
My problem is a strange deflection that is shown in the solutions spot and I do not know what could be the reason of it. I don't know if is because of the boundary conditions or maybe a bad laminate configuration.
I wii be very thankful for any help. I attached a few photos that could help in the understanding of the problem.
Thank you in advance.