We’re updating our badges platform. Badge issuance is temporarily paused, but all completions are being recorded and will be fulfilled once the platform is live. Thank you for your patience.
General Mechanical

General Mechanical

Topics related to Mechanical Enterprise, Motion, Additive Print and more.

Tensile Test on composite panel

    • FahadShafi
      Subscriber

      Hey, I am doing tensile test simulation on carbon fiber epoxy resin composite panel. In the standard test, a rate of displacement 2mm/min is applied, should I apply 2mm displacement in static structural or should I consider displacement for one second?

    • peteroznewman
      Subscriber
      nYou can apply the 2 mm displacement in 1 second in Static Structural.n
    • FahadShafi
      Subscriber
      nI am trying to figure out the tensile strength of the composite panel and how does fiber misalignment influences it. The panel here is 2mm thick consisting of 0/4/4/0 degree plies each of 0.5mm. Using ACP PrePost, I applied multiple failure criterias to observe where exactly the ply fractures. For the standard displacement i.e. 2mm, I am getting the following failure contour for the top ply:nI don't know what does th, e1t and e2t stands for. I think from the legend it is safe to conclude that the entire red region has fractured. To find the localised region of failure, Should I reduce the applied displacement ?nLastly, I wanted inquire about the stresses I am getting. In my opinion, these values are much higher.nWhat do you think about the stress contour? Have I messed up the boundary conditions ? (I applied fixed support on one tab, applied displacement along x on the other, and constrained the panel displacement in z and y directions)nn
Viewing 2 reply threads
  • The topic ‘Tensile Test on composite panel’ is closed to new replies.