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Showing 1 to 4 of 4 for “"Thin Ply"”.

  1. Local and Global Sensitivity Analysis of Thin Ply Laminated Carbon Composites

    … the strength of laminates constructed from very thin plies. Interlaminar shear and normal stress components have been shown to be concentrated on the edges, the so-called edge effect, of unidirectional laminates at the interface between plies of different fiber orientation. Research has shown …

    vt Repository record for Local and Global Sensitivity Analysis of Thin Ply Laminated Carbon Composites (opens in a new tab)

  2. Effects of Shallow Bi-Angle, Thin-Ply Laminates on the Structural Performance of Composite Wings

    … of mechanical properties that shallow bi-angle, thin-ply laminates bring to fiber reinforced polymer composites. Coupon- and structural-level tests are conducted along with numerical simulations. According to the coupon tests, we find that shallow bi-angle fibers and thin plies can increase the …

    washington Repository record for Effects of Shallow Bi-Angle, Thin-Ply Laminates on the Structural Performance of Composite Wings (opens in a new tab)

  3. X-ray Micro-Computed Tomography and Deep Learning Segmentation of Progressive Damage in Hierarchical Nanoengineered Carbon Fiber Composites

    … generally as polymer matrix cracking within (intralaminar) and between (interlaminar, termed ‘delamination’) plies, fiber fracture, fiber bundle microbuckling, and fiber/matrix interfacial debonding. Two emerging solutions aiming to suppress or delay such mechanisms toward enhanced …

    mit Repository record for X-ray Micro-Computed Tomography and Deep Learning Segmentation of Progressive Damage in Hierarchical Nanoengineered Carbon Fiber Composites (opens in a new tab)

  4. The Effect of Part Curvature on the Formation of Residual Stresses in Carbon Fiber Prepreg Laminates

    … and [45/-45]<sub>2</sub>, and two using thin plies, [0/90]<sub>3s</sub> and [45/-45]<sub>6.</sub> The strains that develop during the cure cycle are measured using the DIC and temperature dependent modulus data is obtained using Dynamic Mechanical Analysis (DMA). Utilizing these, the …

    embry-riddle Repository record for The Effect of Part Curvature on the Formation of Residual Stresses in Carbon Fiber Prepreg Laminates (opens in a new tab)