The scratch 2D twill carbon fiber-reinforced-polymer (CFRP) removal and surface evolution mechanism was studied with single abrasive scratch experiments, and the single abrasive scratch finite element model (FEM) was constructed considering progressive damage models. The surfaces evolution mechanism are revealed by FEM stress field analysis and by scanning electron microscope (SEM) images. There is weft -warp fiber woven coupling structure inside 2D twill CFRP, in this paper, woven structure coupling effect means the impedance force fields are formed by the other adjacent carbon fibers during single abrasive scratching weft or warp fibers inside CFRP. The FEM stress fields for the fiber bundles, interfaces and matrices can be analyzed, and provide an effective way to study scratch damage mechanism. Scratch damage mode for weft-containing CFRP starts with resin matrix cracks under low stress as the main feature, gradually transits to carbon fiber pull-out due to stress above interface strengthen and matrix cracks as the main features, and the damage modes finally characterize with weft carbon fibers breakage due to stress above carbon fiber shear fracture strength, fiber pull-out and matrix breakage as the main features. Scratches damage mode for warp-containing starts with the resin matrix breakage, woven structure coupling effect results in fibers stress above the tensile strength, and scratches damage mode transits to the warp fibers pull-out damage and warp carbon fibers breakage as the main features. By comparing the FEM to experimental results for scratch force and SEM, the FE model proves to be valid and accuracy.
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