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  1. Searc

    Choosing FE Simulation Type for Dynamics and Impact/Force Data into FE

    Thanks for the reply FEA way. Just for context, this is a wheelchair hitting a wall and not a car crashing into a wall. The stresses and deformations are low, hence, why I was thinking of Linear Dynamic (Modal Time History) or even linear static given the 'if the frequency of a load is larger...
  2. Searc

    Choosing FE Simulation Type for Dynamics and Impact/Force Data into FE

    Thanks Greg, The peak impact force being Fmax = (m * v^2) / s ? Which is twice the average force = (½ m v^2) / s
  3. Searc

    Choosing FE Simulation Type for Dynamics and Impact/Force Data into FE

    I am running the FEA of a wheel hitting a wall and trying to determine whether I have to use a dynamical simulation, or whether a static simulation can give reasonable results instead. I am interested in the stresses and deformation of the wheel parts. Question 1 The Solidworks Simulation help...
  4. Searc

    Build up a business where you consult / contract as a mechanical designer (UK)

    I am currently a mechanical design engineer contractor PAYE through an agency (UK). Speaking with a colleague at work where his contract is coming to an end. His plan is to only take on roles through his personal service company and build up a group of clients over time. His plan is to...
  5. Searc

    Simulation of Non-layered Composite

    Hi FEA way and SWComposites - thanks for the help btw. I'm having a look at Moldflow, Moldex3D and Fibersim. I think the best current method I have available now is to either use a low number of thick plies and extrude into a solid elements within Ansys ACP, or use oriented elements with...
  6. Searc

    Simulation of Non-layered Composite

    Hi SWComposites, thanks for the reply. Is there another approach you would suggest, instead? Perhaps in another piece of software? Or is it a problem without a current solution which can only be solved with testing & validation? Additionally, if the failure theories in Anaya are not...
  7. Searc

    Simulation of Non-layered Composite

    So I am looking at the method in general, but I will try to give you an idea of the type of parts if could be used for - these are just generic examples. https://st.mascus.com/imagetilewm/product/hso/volvo-link-arm-volvo-l180e,99295602_1.jpg The fibre could be UD down the length of the arm and...
  8. Searc

    Simulation of Non-layered Composite

    Not sure I understand because as the fibre direction changes over the part the isotropic properties stiffest direction changes too. So unless you were modelling a part with no fibre direction change you would need the mesh element directions to change over the part volume.
  9. Searc

    Simulation of Non-layered Composite

    Please could you go into further detail about the macroscale approach you mentioned? My current approach to this method is to model and mesh in normal 3D, then orient each element to have the macro-orthotropic properties in the correct direction for the fibre direction at that point in the...
  10. Searc

    Simulation of Non-layered Composite

    Thanks for the reply FEA way. Hmm, I think method is good if you have say up to 20 fibres through a volume, but in this case it is thousands plus tows. Additionally, though I may know the general placement and path of a group of fibres, each fibre may deviate. I have test data for the composite...
  11. Searc

    Simulation of Non-layered Composite

    Hi there, The composite I am looking to simulate has long fibre cast into a matrix (metal-matrix-composite), and is not layered up like an epoxy-carbon. The fibres are sometime uni-directional and sometime follow a 3D path. The 'traditional' approach for composite FEA is to model the plies on...
  12. Searc

    Defining Datum at mid-plane between none parallel surfaces (GD&T)

    Hey, I am trying to finalise a machining drawing of a part shown in it's finish state here: https://postimg.cc/DWDPQcYm. The part is made via an unusual casting process - the part is cast between two plates, which once removed only leaves the middle profile surface (labelled A) and end surface...
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