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! get inertia about CG & mass | |
*get, mass_x, ELEM,0,MTOT,X | |
*get, mass_y, ELEM,0,MTOT,Y | |
*get, mass_z, ELEM,0,MTOT,Z | |
*get, cg_x, ELEM,0,MC,X | |
*get, cg_y, ELEM,0,MC,Y | |
*get, cg_z, ELEM,0,MC,Z | |
*get, moim_x, ELEM,0,IMC,X | |
*get, moim_y, ELEM,0,IMC,Y | |
*get, moim_z, ELEM,0,IMC,Z | |
*get, moim_xy, ELEM,0,IMC,XY | |
*get, moim_yz, ELEM,0,IMC,YZ | |
*get, moim_zx, ELEM,0,IMC,ZX | |
! translate inertia components to cs_mass loc | |
xg = cg_x - cs_x | |
yg = cg_y - cs_y | |
zg = cg_z - cs_z | |
Ixx_cst = moim_x+mass_x*(yg**2+zg**2) | |
Iyy_cst = moim_y+mass_y*(xg**2+zg**2) | |
Izz_cst = moim_z+mass_z*(xg**2+yg**2) | |
Ixy_cst = moim_xy+mass_x*xg*yg | |
Iyz_cst = moim_yz+mass_y*yg*zg | |
Izx_cst = moim_zx+mass_z*zg*xg | |
! create APDL 2D array | |
*dim,I_cst, array,3,3 | |
I_cst(1,1)=Ixx_cst | |
I_cst(1,2)=Ixy_cst | |
I_cst(1,3)=Izx_cst | |
I_cst(2,1)=Ixy_cst | |
I_cst(2,2)=Iyy_cst | |
I_cst(2,3)=Iyz_cst | |
I_cst(3,1)=Izx_cst | |
I_cst(3,2)=Iyz_cst | |
I_cst(3,3)=Izz_cst |
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