I do not know whether I am posting my concerns in the right forum or not. I am a aircraft structural engineer. I always encounter new or updated loads on wings from aerodynamics.I generally use excel and convert these loads into FE nodal loads.Now I want to write a generalised program for nodal load computation. I want back end computations and fore end inputs as well. What language/ software like python,Fortran, javanet ,visualc++.....etc...can be used to program efficiently .
Thanks in advance.
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