aeroelastic of blade with abaqus
hello
i have a problem,i am trying it about one years
is:aeroelastic blade of helicopter with abaqus
i find some method for solution:
1.using abaqus for 2D ANALYSIS of cross section(meshed cross section) and then 1D modal analysis modal,then using ZAERO for aerodynamic load,my problem in case is:linking abaqus and zaero.what is solutin method?