Based　on　the　Timoshenko-Mindlin　theory,　strain　energy　equivalence　hypothesis　and　Boltzmann　super-position　principle,　the　nonlinear　creep-damage　equilibrium　equations　of　cross-ply　laminated　cylindrical　panels　subjected　to　an　axially　compressive　load　are　established　under　considering　geometric　nonlinearity,　transverse　shear　deformation,　damage　effect　and　initial　imperfection.　The　damage　evolution　equation　proposed　by　Kachanov　is　taken,　but　considering　the　tension　and　compression　have　different　contribution　to　the　rate　of　the　material＇s　damage　evolution.　In　the　numerical　calculations,　the　influences　of　various　parameters　including　transverse　shear　deformation,　geometric　parameter　and　number　of　layers　on　the　creep　postbuckling　behavior　of　damage/viscoelastic　laminated　cylindrical　panels　and　damage　evolution　property　are　discussed　in　detail.