[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

Littell et al., 2009 - Google Patents

Effect of microscopic damage events on static and ballistic impact strength of triaxial braid composites

Littell et al., 2009

View HTML
Document ID
8962210027627371333
Author
Littell J
Binienda W
Arnold W
Roberts G
Goldberg R
Publication year
Publication venue
Composites Part A: Applied Science and Manufacturing

External Links

Snippet

The reliability of impact simulations for aircraft components made with triaxial braided carbon fiber composites is currently limited by inadequate material property data and lack of validated material models for analysis. Methods to characterize the material properties used …
Continue reading at www.sciencedirect.com (HTML) (other versions)

Classifications

    • GPHYSICS
    • G06COMPUTING; CALCULATING; COUNTING
    • G06FELECTRICAL DIGITAL DATA PROCESSING
    • G06F17/00Digital computing or data processing equipment or methods, specially adapted for specific functions
    • G06F17/50Computer-aided design
    • G06F17/5009Computer-aided design using simulation
    • G06F17/5018Computer-aided design using simulation using finite difference methods or finite element methods

Similar Documents

Publication Publication Date Title
Zhao et al. Modeling the transverse tensile and compressive failure behavior of triaxially braided composites
Zhang et al. Progressive damage simulation of triaxially braided composite using a 3D meso-scale finite element model
Hu et al. Integrated XFEM-CE analysis of delamination migration in multi-directional composite laminates
Zhang et al. A meso-scale finite element model for simulating free-edge effect in carbon/epoxy textile composite
Short et al. The effect of delamination geometry on the compressive failure of composite laminates
Littell et al. Effect of microscopic damage events on static and ballistic impact strength of triaxial braid composites
Zhang et al. Experimental and FEM study of thermal cycling induced microcracking in carbon/epoxy triaxial braided composites
Goldberg et al. Modification of a macromechanical finite element–based model for impact analysis of Triaxially braided composites
Rashedi et al. Fracture characterization of glass fiber composite laminate under experimental biaxial loading
Krueger et al. Fatigue life methodology for bonded composite skin/stringer configurations
Orifici et al. A finite element methodology for analysing degradation and collapse in postbuckling composite aerospace structures
Hu et al. Stress analysis and damage evolution in individual plies of notched composite laminates subjected to in-plane loads
Caous et al. A method to determine composite material residual tensile strength in the fibre direction as a function of the matrix damage state after fatigue loading
Huang et al. Statistical analysis of oblique crack evolution in composite laminates
Zhang et al. Compressive strength determined for ultrahigh modulus fiber reinforced composites by [90/0] ns laminates
Cater et al. Experimental and numerical analysis of triaxially braided composites utilizing a modified subcell modeling approach
Cheng Material modeling of strain rate dependent polymer and 2D tri-axially braided composites
Smith et al. Applications of ultrasonic NDT to aerospace composites
Roberts et al. Characterization of triaxial braided composite material properties for impact simulation
Farrokhabadi et al. Assessment of delamination growth due to matrix cracking in hybrid Glass-Kevlar composite laminates using experimental, numerical and analytical methods
Arellano et al. Strain field measurement of filament-wound composites at±55 using digital image correlation: an approach for unit cells employing flat specimens
Nikishkov et al. Simulation of damage in composites based on solid finite elements
Pradhan et al. The influence of ply sequence and thermoelastic stress field on asymmetric delamination crack growth behavior of embedded elliptical delaminations in laminated FRP composites
Goldberg et al. Investigation of a macromechanical approach to analyzing triaxially-braided polymer composites
CRUZ et al. Effect of thermal residual stresses on buckling and post-buckling properties of laminated composites perimetrally reinforced