In　this　study,　the　adiabatic　film　cooling　effectiveness　and　conjugate　heat　transfer　characteristics　for　a　circular　hole　are　investigated　numerically.　Seven　turbulator　ribs　are　located　on　the　internal　wall,　and　a　film　cooling　hole　between　two　adjacent　ribs　has　an　inclination　angle　of　30　degrees.　The　secondary　flow　rate　is　affected　by　the　internal　channel　flow　velocity,　and　the　external　film　cooling　is　combined　with　the　internal　channel　flow　conditions.　In　the　conjugate　heat　transfer　research,　two　different　plate　materials　are　considered　to　analyze　the　heat　conduction　characteristics.　The　results　show　that　the　turbulator　ribs　enhance　the　downstream　heat　transfer　and　provide　a　more　extensive　coverage　area　and　effective　cooling　protection.　More　blade-wall　heat　is　transferred　by　heat　conduction,　which　makes　the　area-average　wall　temperature　for　the　high　thermal　conductivity　case　to　decrease　along　the　secondary　flow　direction.　The　wall　temperature　distribution　and　film　cooling　effectiveness　are　affected　significantly　by　heat　conduction.