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Showing 1 to 15 of 15 for “"progressive failure analysis"”.

  1. Progressive failure analysis of laminated composite structures

    A methodology for progressive failure analysis is presented that is applicable to thin composite structures undergoing large deformations. The method is based on a nonlinear shell theory that accounts for geometric and material nonlinearities. An isoparametric, displacement-based finite element …

    vt Repository record for Progressive failure analysis of laminated composite structures (opens in a new tab)

  2. Progressive Failure Analysis of Laminated Composite Structures

    … composite structures requires a complete failure analysis, which includes both initiation and propagation of damage. In this work a progressive failure methodology is developed and implemented in the commercial Finite Element software package, Abaqus. Out of the numerous failure criteria …

    vt Repository record for Progressive Failure Analysis of Laminated Composite Structures (opens in a new tab)

  3. Progressive Failure Analysis of Double-Notched Composite Laminates

    Failure analysis in composite laminates is traditionally modeled by the material property degradation method for the in-plane damage prediction which assumes that a damage material can be replaced by an equivalent material with degraded properties. The delamination in composites, on the other hand, …

    nus Repository record for Progressive Failure Analysis of Double-Notched Composite Laminates (opens in a new tab)

  4. Comprehensive Multi-Scale Progressive Failure Analysis for Damage Arresting Advanced Aerospace Hybrid Structures

    … level. Therefore, a computational methodology is progressively developed based on physically realistic concepts without the use of tuning parameters. A thorough verification study is performed to identify the most effective approach to model PRSEUS, including the effect of element type, boundary …

    vt Repository record for Comprehensive Multi-Scale Progressive Failure Analysis for Damage Arresting Advanced Aerospace Hybrid Structures (opens in a new tab)

  5. Optimal design of composite fuselage frames for crashworthiness

    … for increasing structural crashworthiness is a progressive failure analysis. Currently, the most widely used analysis methods for progressive failure of composite structures are considered too expensive computationally for practical optimization in today's computing environment. Developing an …

    vt Repository record for Optimal design of composite fuselage frames for crashworthiness (opens in a new tab)

  6. Failure Initiation and Progression in Internally Pressurized Non-Circular Composite Cylinders

    In this study, a progressive failure analysis is used to investigate leakage in internally pressurized non-circular composite cylinders. This type of approach accounts for the localized loss of stiffness when material failure occurs at some location in a structure by degrading the local material …

    vt Repository record for Failure Initiation and Progression in Internally Pressurized Non-Circular Composite Cylinders (opens in a new tab)

  7. Nonlinear analysis of laminated composite shells using a micromechanics-based progressive damage model

    A micromechanics-based model for progressive failure analysis of laminated composite shell structures has been developed and implemented. The model couples a finite element model for nonlinear analysis of laminated shells with a micro mechanics elasticity solution for predicting failure and …

    vt Repository record for Nonlinear analysis of laminated composite shells using a micromechanics-based progressive damage model (opens in a new tab)

  8. Finite Element Analysis of Defects in Cord-Rubber Composites and Hyperelastic Materials

    … finite element approach based on the multiscale progressive failure analysis is employed to provide the theoretical predictions for damage development in the cord-rubber composites in tires. This new three-dimensional model of the cord-rubber composite is proposed to predict the different types …

    vt Repository record for Finite Element Analysis of Defects in Cord-Rubber Composites and Hyperelastic Materials (opens in a new tab)

  9. Compression After Impact Experiments and Analysis on Honeycomb Core Sandwich Panels with Thin Facesheets

    … in the areas of experimental testing, and analysis methods. A set of experiments on Nomex honeycomb core sandwich panels, with thin woven fiberglass cloth facesheets, is described, which includes detailed instrumentation and unique observation techniques. These techniques include high speed …

    vt Repository record for Compression After Impact Experiments and Analysis on Honeycomb Core Sandwich Panels with Thin Facesheets (opens in a new tab)

  10. Torsion of Elliptical Composite Cylindrical Shells

    … responses are examined, and material failure is considered. Four elliptical cross sections, defined by their aspect ratio, the ratio of minor to major radii, are considered: 1.00 (circular), 0.85, 0.70, and 0.55. Two overall cylinder sizes are studied; a small size with a radius and …

    vt Repository record for Torsion of Elliptical Composite Cylindrical Shells (opens in a new tab)

  11. Optimal Parameters for Doubly Curved Sandwich Shells, Composite Laminates, and Atmospheric Plasma Spray Process

    … stress recovery scheme (SRS) and the Tsai-Wu failure criterion to find the stacking sequence of composite laminates and the topology and materials for doubly curved sandwich shells to maximize the first failure load. It is followed by the progressive failure analysis to determine the ultimate …

    vt Repository record for Optimal Parameters for Doubly Curved Sandwich Shells, Composite Laminates, and Atmospheric Plasma Spray Process (opens in a new tab)

  12. Finite element-based failure analysis of composite laminates with non-destructive feature quantification.

    … very difficult to characterize and predict the failure process while they are in operation. This research experimentally investigates the failure mechanism of CFRP manufactured under three different loading modes: failure onset for a planar loading condition, delamination for a mixed mode static …

    baylor Repository record for Finite element-based failure analysis of composite laminates with non-destructive feature quantification. (opens in a new tab)

  13. Optimum First Failure Loads of Sandwich Plates/Shells and Vibrations of Incompressible Material Plates

    … face sheets for it to have the maximum first failure load under quasistatic (blast) loads. The analyses employ a third-order shear and normal deformable plate/shell theory (TSNDT), the finite element method (FEM), a stress recovery scheme (SRS), the Tsai-Wu failure criterion and the Nest-Site …

    vt Repository record for Optimum First Failure Loads of Sandwich Plates/Shells and Vibrations of Incompressible Material Plates (opens in a new tab)

  14. Analytical Modeling of the Mechanics of Nucleation and Growth of Cracks

    … literature and those developed in this work. A progressive failure methodology is developed and demonstrated to simulate the initiation and material degradation of a laminated panel due to intralaminar and interlaminar failures. Initiation of intralaminar failure can be by a matrix-cracking …

    vt Repository record for Analytical Modeling of the Mechanics of Nucleation and Growth of Cracks (opens in a new tab)