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Found 4 results

  1. Hi, Does anyone have any tips on how to go about optimising the internal structure of an aircraft wing? I am a very new user to Hypermesh. Thanks.
  2. Hi all, I've been trying to get a wing model from HM to VWT. I've been told that the body I've created thus far is correct (see bottom of post). What I've done is clean up the geometry and created a solid from the bounding surfaces. However, no matter what mesh I create (surface deviation, CFD tetra, etc) when I import into VWT (CFD>Nastran Fluent) there isnt one single volume but four separate ones. This seems to fail when I run the analysis. Can anyone point me in the right direction. Regards, A. John Baker HM wing model: https://www.dropbox.com/s/5hqmijj3ifwkdi6/defeatured_model%20%281%29.hm
  3. Hi, I am new to Hypermesh and am trying to analyse the load that will be exerted on the airfoil based on the pressure distribution along the airfoil (refer to pic). Is it possible to import these values from the graph into hypermesh?
  4. I'm trying to apply pressure loads on an aircraft wing. I've created a .csv file for the same . the first column of the file represents the wing chord, second column represents the wing span and the third represents the pressure magnitude(figure attached). When I apply this load on the wing, the pressure is not applied normal to the elements (figure attached). I've checked the element normals and they all point outward. I'm not able to figure out why the pressure is not being applied in the normal direction. Please suggest solutions. Thanks.
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