Under nonproportional loading, the principal planes of material, stress and
damage are expected to differ, producing a hysteretic effect on the result
ing design and failure analysis. This paper describes the development of an
anisotropic damage model taking into account the effect of the principal d
amage plane rotation. All of the required mathematical formulations to gene
ralize the damage model are derived in the principal damage coordinate syst
em. Numerical procedures to include the changing damage planes are describe
d in details. Two example cases of AL6111-T4 sheet material are provided to
demonstrate the importance of the rotational effects of the principal plan
es on the resulting material behaviors under nonproportional loading.