Dear 2288,
it will b better if u specify what all variables u have the values with u. And what d u want to calculate ?? That will help in giving u the xact solution.
Sanab.
Hi Blues
i m in the same boat. But i m using Panel Method(VLM) for Aerodynamics. I have written a Fortran program on the guidelines given the MSC/NASTRAN manual. But still the Question is how one can transfer the pressure loads of CFD to nodal loads of FEM both having different meshes. Since...