Internal forces:
Loads operating in surface of system: $obc$
Section location: a=$Odpocz$ m, b=$Odkon$ m,
Bending moments: Mx=$MomX$ kNm, My=$MomY$ kNm,
Transversa forces: Qy=$PopY$ kN, Qx=$PopX$ kN,
Axial force: N=$Osiowa$ kN, (*Ms
Statical excentrics ex=-My/N=-($MomY$)/($Osiowa$)=$Wex$ m,
ey=Mx/N=($MomX$)/($Osiowa$)=$Wey$ m*)(*USU
Regard to member slenderness ratio in surface of system:
Mx=hx (eny + esy) N =$FMoU$ kNm,*)(*USP
Regard to member slenderness ratio in surface perpendicular of system:
My=hy (enx + esx) N =$FMoP$ kNm*).
greglagozny