sdl q0*sin(pi*X/a)*sin(pi*Y/a) "Sinusoidal distributed transverse load"
SXX_lw lshell.SXX/q0*(th/a)^2 "In-plane normal stress (SXX), normalized"
SZZ_lw lshell.SZZ/q0 "Transverse normal stress (SZZ), normalized"
SYZ_lw lshell.SYZ/q0*th/a "Transverse shear stress (SYZ), normalized"
SXZ_lw lshell.SXZ/q0*th/a "Transverse shear stress (SXZ), normalized"
SXX_esl shell.SXX/q0*(th/a)^2 "In-plane normal stress (SXX), normalized"
SZZ_esl shell.SZZ/q0 "Transverse normal stress (SZZ), normalized"
SYZ_esl shell.SYZ/q0*th/a "Transverse shear stress (SYZ), normalized"
SXZ_esl shell.SXZ/q0*th/a "Transverse shear stress (SXZ), normalized"
A 1.105*a/2 "Cut point coordinate"
B 1.894*a/2 "Cut point coordinate"