Massively　parallel　simulation　based　on　hybrid　thermal　lattice　Boltzmann　method　(HTLBM)　is　performed　to　analyze　the　near-wall　flow　and　heat　transfer　characteristics　in　compound　angled　film　cooling.　Multiple　graphic　processing　units　(Multi-GPUs)　are　used　to　speed　up　the　computations.　The　effect　of　compound　angle　on　the　instantaneous　flow　characteristics　and　cooling　performance　with　various　blowing　ratios　and　inclined　angles　are　studied　in　detail.　In　the　simulation,　three　compound　angles　of　beta　=　15　degrees,　30　degrees,　450　degrees　are　considered.　The　inclined　angles　of　coolant　jet　to　the　flat　surface　are　set　to　alpha=　30　and　alpha　=　600,　respectively.　The　blowing　ratios　are　BR　=　0.5　and　BR　=　1.0.　It　is　observed　that　the　application　of　compound　angle　enhances　the　mixing　between　the　crossflow　and　the　jet　flow,　especially　for　the　large-blowing-ratio　cases.　The　detachment　of　the　coolant　jet　is　reduced　by　applying　compound　angle,　which　results　in　the　increasing　of　film　cooling　effectiveness,　particularly　in　the　case　of　small　jet　inclined　angle　a.　Moreover,　to　reasonably　evaluate　the　uniformity　of　coolant　film　in　compound　angled　film　cooling,　a　novel　coefficient　(COU)　affording　a　wide　application　is　proposed　in　the　present　work.　The　results　show　that　the　coolant-film　uniformity　is　decreased　by　the　application　of　compound　angle.　(C)　2017　Elsevier　Ltd.　All　rights　reserved.