Numerical investigation of the vertex flow characteristics on double-delta wing was presented. The flows over the 76/40-deg double-delta wing were computed with complete laminar when attack angles varies from 5-deg to 30-deg. The flow structures were exhibited in different angles and the analysis of the aero-dynamic characteristics was presented. The investigation shows that vortexes on the double-delta wing surface may fiercely interact with each other and the burst of vortexes caused by large attack angle will exert great influence on the aero-dynamic characteristics of double-delta wing.