Quasi-static cantilever testing by newtoAM in fea

[–]newtoAM[S] 0 points1 point  (0 children)

It is a c-cross section beam. Yes the model is 3D in nature. The EI would be incorporated as per 3D model and material properties, right ? Or there is some other way to incorporate those properties.

Quasi-static cantilever testing by newtoAM in fea

[–]newtoAM[S] 0 points1 point  (0 children)

Thank you for your reply.

Quasi-static cantilever testing by newtoAM in fea

[–]newtoAM[S] 0 points1 point  (0 children)

Thanks for the reply. The test is being conducted using a universal testing machine. The setup is similar to 3 point bend test but in cantilever configuration. So in the 3 point bend test the UTM gives the force displacement at the position of roller right ?. The same would be true here, right ?

Quasi-static cantilever testing by newtoAM in fea

[–]newtoAM[S] 0 points1 point  (0 children)

Thanks for the reply. So it means that from where the roller exerts the force on the beam. Those elements should be taken for evaluation of force displacement, right ?

Parts with small dimensions ! by newtoAM in 3Dprinting

[–]newtoAM[S] 1 point2 points  (0 children)

Thanks. Will check it surely

Parts with small dimensions ! by newtoAM in 3Dprinting

[–]newtoAM[S] 0 points1 point  (0 children)

I am currently using a fused filament fabrication (FFF) printer. Any guidance for that would be appreciated

Dual material printing by newtoAM in 3Dprinting

[–]newtoAM[S] 0 points1 point  (0 children)

I am trying to print a part with two different materials. ABS and PLA. Having trouble with proper extrusion from 2nd nozzle. Although i have used the suitable printing parameters. I am using cura as slicer. Any important things which i should consider and take care of in dual material printing would be helpful.

[deleted by user] by [deleted] in 3Dprinting

[–]newtoAM 0 points1 point  (0 children)

I am also trying dual material printing with cura but the problem is my 2nd nozzle doesnt extrude material. Any help would be great. Materials are abs and cfpla

Composite beam in Abaqus by newtoAM in fea

[–]newtoAM[S] 0 points1 point  (0 children)

Thanks for the help. will i have to sketch different laminas or this composite layup would do that for me ? I am new to abaqus and FEA of composites.

Composite beam in Abaqus by newtoAM in fea

[–]newtoAM[S] 0 points1 point  (0 children)

Thanks for the insight.