I have a swept wing that I made in Solidworks and would like to import it into Fluent so I can run some calculations such as lift and drag and various coefficients. For a 2D airfoil is it straight forward, but for a 3D wing it seems a bit more complicated. I have imported the model as a...
I have this solid model of a wing using solid elements and I would like to apply a linear distributed load and eventually a non linear load extending from root to the tip of the wing. I have successfully applied an evenly distributed load from the root to the tip. I simply selected...
I have created a solid model of a wing. It is a NACA 0012 airfoil simply extruded for a span of 10 inches and a chord of 1.5 inches. When I imported the model into FeMap as a parasolid, the results of the analysis do not seem to be correct. I believe it is because I meshed it incorrectly. I am...
I have created a solid model of a wing. It is a NACA 0012 airfoil simply extruded along a certain length. When I imported the model into FEMAP as a parasolid, the results of the analysis do not seem to be correct. I believe it is because I meshed it incorrectly. I am getting a unit load...
