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Showing 1 to 20 of 407 for “"Laminates"”.

  1. Phase selective flame-retardant laminates

    … to enhance the fire performance of polymer laminates through structural optimisation and material innovation. The first approach involves applying external protective coatings to carbon fibre-reinforced polymer (CFRP) laminates using three configurations: cellulose nanofibres CNF/clay …

    tu-berlin Repository record for Phase selective flame-retardant laminates (opens in a new tab)

  2. High modulus carbon fiber/titanium laminates

    … low weight materials in the form of composite laminates. In this investigation, laminates were fabricated using inorganic matrix/high modulus carbon fiber composites with titanium sheets. Laminates were tested in three-point bending to assess the performance of the upgrade. The results show …

    mit Repository record for High modulus carbon fiber/titanium laminates (opens in a new tab)

  3. Interlaminar fatigue of fiber-reinforced laminates.

    Thesis: M.S., Massachusetts Institute of Technology, Department of Mechanical Engineering, 1971

    mit Repository record for Interlaminar fatigue of fiber-reinforced laminates. (opens in a new tab)

  4. Edge caps for reinforcing composite laminates

    … of an experimental program are presented. Cappad laminates are shown to be on average 130% to 140%. stronger than uncapped laminates when subjected to static tensile or tension-tension fatigue loading. In addition, the coefficient of variation of the static tensile failure load decreases from 24% …

    vt Repository record for Edge caps for reinforcing composite laminates (opens in a new tab)

  5. Compression failure of angle-ply laminates

    … mechanisms of failure in compression of angleply laminates. Experimental results were obtained from 42 angle-ply IM7/8551-7a specimens with a lay-up of [ (±9) / (=F9)] 6s where 9, the off-axis angle, ranged from 0° to 90°. The results showed four failure modes, these modes being a function of …

    vt Repository record for Compression failure of angle-ply laminates (opens in a new tab)

  6. Long term behavior of Arall laminates

    The behavior of ARALL (ARamid ALuminum Laminates) subjected to tension-tension cyclic loading was experimentally investigated as a first step towards the understanding of the fatigue damage mechanisms in Arall laminates, and the relationships between damage and stiffness change, remaining strength …

    vt Repository record for Long term behavior of Arall laminates (opens in a new tab)

  7. Process-Induced Viscoelastic Stress in Composite Laminates

    … in evaluating the stress response of composite laminates which is associated with cooling the material system from the cure temperature to room temperature. The present research examines the fundamental nature of time-dependent residual-thermal stresses in composite laminates which are caused by …

    uiuc Repository record for Process-Induced Viscoelastic Stress in Composite Laminates (opens in a new tab)

  8. Adhesive properties of thermoset fibre metal laminates

    Fibre metal laminates (FMLs) are composite materials that consist of layers of metal and fibre reinforced polymers. FMLs are used in the construction of aircraft fuselage skins, such as the Airbus A380. GLARE, the only commercially available FML, is of particular interest due to its damage …

    cape-town Repository record for Adhesive properties of thermoset fibre metal laminates (opens in a new tab)

  9. Fatigue damage in titanium graphite hybrid laminates

    Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1998.

    mit Repository record for Fatigue damage in titanium graphite hybrid laminates (opens in a new tab)

  10. Fatigue response of notched graphite--epoxy laminates

    … of notched quasi-isotropic graphite-epoxy laminates were recorded and related to the fatigue damage. Two different laminates [0,90,+45,-45]s (type A) and [ +45, 90, -45, 0] s (type B) were considered and the effects of stacking sequence were compared. Nondestructive testing techniques such …

    vt Repository record for Fatigue response of notched graphite--epoxy laminates (opens in a new tab)

  11. SMA-Induced Deformations In general Unsymmetric Laminates

    General unsymmetric laminates exhibit large natural curvatures at room temperature. Additionally, inherent to most unsymmetric laminates is the presence of two stable configurations. Multiple configurations and stability issues arise because of the geometric nonlinearities associated with the large …

    vt Repository record for SMA-Induced Deformations In general Unsymmetric Laminates (opens in a new tab)

  12. Analysis of Composite Laminates with Matrix Cracks

    … of the effects of matrix cracking on composite laminates is a well-known problem which has attracted considerable attention for the past decade. An approximate analytical solution is introduced in this thesis to study this type of problem. The subjects of primary concern are the degradation of …

    vt Repository record for Analysis of Composite Laminates with Matrix Cracks (opens in a new tab)

  13. Analysis of Tow-Placed, Variable-Stiffness Laminates

    … considered in the analysis of variable-stiffness laminates was limits on fiber curvature which proved to be more restrictive for parallel fiber laminae than for shifted fiber. The in-plane responses of shifted and parallel fiber variable-stiffness laminates to either an applied uniform end …

    vt Repository record for Analysis of Tow-Placed, Variable-Stiffness Laminates (opens in a new tab)

  14. Geometrically Nonlinear Stress Recovery in Composite Laminates

    Composite laminates are increasingly being used as primary load bearing members in<br />structures. However, because of the directional dependence of the properties of<br />composite materials, additional failure modes appear that are absent in<br />homogeneous, isotropic materials. Therefore, a …

    vt Repository record for Geometrically Nonlinear Stress Recovery in Composite Laminates (opens in a new tab)

  15. Delamination initiation in postbuckled dropped-ply laminates

    The compression strength of dropped-ply, graphite-epoxy laminated plates for the delamination mode of failure is studied by analysis and corroborated with experiments. The nonlinear response of the test specimens is modeled by a geometrically nonlinear finite element analysis. The methodology for …

    vt Repository record for Delamination initiation in postbuckled dropped-ply laminates (opens in a new tab)

  16. Strength in notched and impact damaged laminates

    The strength of notched and impact damaged laminates was studied. The solution for a plate containing an elliptic opening and inclusion was used as given by Lekhnitskii. The solution for the infinite plate, combined with laminate analysis to determine the ply stresses, and the average stress …

    vt Repository record for Strength in notched and impact damaged laminates (opens in a new tab)

  17. Characterization of Bistability Behavior in Unsymmetric CFRP Laminates

    <p>Composite laminates of unsymmetric layup families often exhibit twin stable shapes at room temperature, a phenomenon known as bistability. Unsymmetric bistable composite laminates have often been suggested for applications in aerospace morphing structures, damping, and energy storage, because of …

    embry-riddle Repository record for Characterization of Bistability Behavior in Unsymmetric CFRP Laminates (opens in a new tab)

  18. Nonlinear Analysis of Unsymmetric Laminates under Cylindrical Bending

    … analysis of unsymmetric composite long, narrow laminates under cylindrical bending is studied. The nonlinear governing equations are obtained to analyze the cylindrical bending of arbitrary laminates. The <em>von-Karman</em> type geometrical nonlinearity is incorporated in the governing …

    embry-riddle Repository record for Nonlinear Analysis of Unsymmetric Laminates under Cylindrical Bending (opens in a new tab)

  19. Analysis of shear test methods for composite laminates

    … specimen is studied for three graphite-epoxy laminates ([0], [90], [±45]<sub>S</sub>); the cross beam is studied for two graphite-epoxy laminates ([0/90]<sub>S</sub>, [±45]<sub>S</sub>); the Iosipescu and rail shear specimens are studied with several materials (steel, graphite-epoxy, and …

    vt Repository record for Analysis of shear test methods for composite laminates (opens in a new tab)

  20. Large strain flexural testing of thin composite laminates

    … space structures. Elastically folded thin laminates can be utilized as hinge mechanisms in structural systems such as solar arrays, reflectors, and instrument booms, allowing for compact packaging during launch to orbit. While the initiative to utilize composite laminates in deployable …

    unm Repository record for Large strain flexural testing of thin composite laminates (opens in a new tab)

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