General Mechanical

General Mechanical

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Boundary condition dilemma

    • itsme_tilak
      Subscriber

      I am simulating the thermal stress developed in a rocket nosecone due to the temperature but I have no idea which boundary condition to apply. Can anyone please give me an idea?  

    • peteroznewman
      Subscriber

      Put a Remote Displacement, Behavior = Deformable on the back circular face of the rocket. Set all six DOF to 0.  The thermal expansion will be relative to a point at the center of that face. You have the imported temperature load already, which is the other boundary condition.

      • itsme_tilak
        Subscriber

        It worked. Thank you so much.

    • peteroznewman
      Subscriber

      You could also put an external Pressure load on the nose cone that comes from a CFD solution.

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