Tensile test of composite layup Materials using abaqus hashin's failure

[@abhishekrai3342]

you are doing great work, but it would be great if you add explanation or sound written text anything to explain it. it would help for beginners to understand.

[@mahaelsaeid3713]

hi could you please explain how to add cohesive behavior between the plyies after specifying the composite layup and without making them separate bodies ?

[@adarshnataraj7904]

Can the stress distribution in Composite layups can be measured using Von Mises stresses? Should we not use Stress components (S11, S12, S23, etc.)?

[@narendrakumarjha5685]

strain 0.000154128 tensile strength as 1.37874 MPa this is the tensile data i obtained performing test on gfrp composite i dont know why i am getting so leeser value material properties are: E11=8943.066, E22=8941.682, E33=41396.052 and one more thing is that during experiment i have applied strain rate of 1mm/min but in abaqus i feed load as a velocity of 1/60 mm/sec is is okay

[@zahidrana6200]

Can you specify the material used in this video

[@ariellusty3193]

th-cam.com/video/F8S842sCfpg/w-d-xo.html

[@algeriayoutube6915]

great work bro

[@ABAQUS_SIMULATION]

thank you.
don't forget subscribe in my youtube chanel for more interesting videos

[@mahaelsaeid3713]

@@ABAQUS_SIMULATION hi could you please explain why did you choose conventional shell for the layup and not continuum shell as usual ?

[@mahaelsaeid3713]

and could you please expaling the purpose of creating those nodes Gauge 1, gauge 2 ?

[@chinmaykabi]

Could you specify the values you used in the material

[@ariellusty3193]

th-cam.com/video/F8S842sCfpg/w-d-xo.html

[@3dmdavid]

thanks! Could you please do it for 3d solid element? Continum shell