Skip to main content

Page of 4
and
  1. No Access

    Article

    The Elastic-Plastic Finite Element Alternating Method (EPFEAM) and the prediction of fracture under WFD conditions in aircraft structures

    This report provides a summary of the Elastic- Plastic Finite Element Alternating Method (EPFEAM), the T *-integral fracture mechanics parameter, and the use of both the tools to predict the residual strength of...

    L. Wang, F. W. Brust, S. N. Atluri in Computational Mechanics (1997)

  2. No Access

    Article

    The Elastic-Plastic Finite Element Alternating Method (EPFEAM) and the prediction of fracture under WFD conditions in aircraft structures

     This report provides a summary of the Elastic-Plastic Finite Element Alternating Method (EPFEAM), the T* -integral fracture mechanics parameter, and the use of both tools to predict the residual strength of airc...

    L. Wang, F. W. Brust, S. N. Atluri in Computational Mechanics (1997)

  3. No Access

    Article

    The Elastic-Plastic Finite Element Alternating Method (EPFEAM) and the prediction of fracture under WFD conditions in aircraft structures

    This report provides a summary of the Elastic-Plastic Finite Element Alternating Method (EPFEAM), the T* -integral fracture mechanics parameter, and the use of both tools to predict the residual strength of a...

    L. Wang, F. W. Brust, S. N. Atluri in Computational Mechanics (1997)

  4. No Access

    Article

    A computational model for analysing interactive buckling and delamination growth in composite structures

    In this paper, a unified method is presented: (i) to model delaminated stiffened laminated composite shells; (ii) for synthesising accurate multiple post-buckling solution paths under compressive loading; and ...

    B P Naganarayana, S N Atluri in Sadhana (1996)

  5. No Access

    Article

    Prediction of post-buckling strength of stiffened laminated composite panels based on the criterion of mixed-mode stress intensity factors

    An analytical investigation is conducted to predict the post-buckling strength of laminated composite stiffened panels under compressive loads. When a stiffened composite panel buckles, the skin would deform i...

    W. T. Chow, S. N. Atluri in Computational Mechanics (1996)

  6. No Access

    Article

    Near-tip fields and intensity factors for interfacial cracks in dissimilar anisotropic piezoelectric media

    A complete form of stress and electric displacement fields in the vicinity of the tip of an interfacial crack, between two dissimilar anisotropic piezoelectric media, is derived by using the complex function t...

    H. G. Beom, S. N. Atluri in International Journal of Fracture (1996)

  7. No Access

    Article

    Finite element calculation of stress intensity factors for interfacial crack using virtual crack closure integral

    This paper presents a successful implementation of the virtual crack closure integral method to calculate the stress intensity factors of an interfacial crack. The present method would compute the mixed-mode s...

    W. T. Chow, S. N. Atluri in Computational Mechanics (1995)

  8. No Access

    Article

    Development of new spatially curved frame finite element for crash analysis part 1: Formulation and validation

    This paper deals with the development of a new space curved frame finite element to be used for crash analysis (non-linear). The formulation has been validated for problems of large deflection and rotation, an...

    S. Vasudevan, H. Okada, S. N. Atluri in Computational Mechanics (1995)

  9. No Access

    Article

    An implementation of the Schwartz-Neumann Alternating Method for collinear multiple cracks with mixed type of boundary conditions

    This paper presents an implementation of the Schwartz-Neumann Alternating Method for multiple collinear cracks with mixed types of boundary conditions. Numerical examples are also presented to show the effecti...

    L. H. Wang, S. N. Atluri in Computational Mechanics (1995)

  10. No Access

    Article

    Residual strength prediction for aircraft panels with Multiple Site Damage, using the “EPFEAM” for stable crack growth analysis

    In this paper, a new analytical method for solving stable crack propagation problems in a ductile panel with a row of cracks, is presented. The main purpose of the present study is to estimate the maximum load...

    C. R. Pyo, H. Okada, S. N. Atluri in Computational Mechanics (1995)

  11. No Access

    Article

    Strength reduction and delamination growth in thin and thick composite plates under compressive loading

    In this paper, the coupled local-global buckling behavior in laminated composite plates with elliptic delaminations and the associated mechanisms of delamination growth under compressive loads are critically e...

    B. P. Naganarayana, S. N. Atluri in Computational Mechanics (1995)

  12. No Access

    Article

    An elastic-plastic finite element alternating method for analyzing wide-spread fatigue damage in aircraft structures

    In this paper, a new analytical technique to study the effect of wide-spread fatigue damage in ductile panels is presented. The main purpose of the study is to develop an efficient methodology to predict the m...

    C. R. Pyo, H. Okada, S. N. Atluri in Computational Mechanics (1995)

  13. No Access

    Article

    Dependence of stress on elastic constants in an anisotropic bimaterial under plane deformation; and the interfacial crack

    Nondimensional parameters that are needed to describe the stress field in an anisotropic bimaterial with tractions prescribed on its boundary are investigated. Two real matrices, which play an important role i...

    H. G. Beom, S. N. Atluri in Computational Mechanics (1995)

  14. No Access

    Article

    Analysis of edge stresses in composite laminates under combined thermo-mechanical loading, using a complementary energy approach

    An approximate method is presented to investigate the interlaminar stresses near the free edges of composite laminate plates that are subjected to a combined thermo-mechanical loading. The method is based upon...

    T. Kim, S. N. Atluri in Computational Mechanics (1995)

  15. No Access

    Article

    Calculation of stress intensity factors for an interfacial crack between dissimilar anisotropic media, using a hybrid element method and the mutual integral

    Using Beom and Atluri's complete eigen-function solutions for stresses and displacements near the tip of an interfacial crack between dissimilar anisotropic media, a hybrid crack tip finite-element is develope...

    W. T. Chow, H. G. Beom, S. N. Atluri in Computational Mechanics (1995)

  16. No Access

    Article

    Rotations in computational solid mechanics

    A survey of variational principles, which form the basis for computational methods in both continuum mechanics and multi-rigid body dynamics is presented: all of them have the distinguishing feature of making ...

    S. N. Atluri, A. Cazzani in Archives of Computational Methods in Engineering (1995)

  17. No Access

    Article

    Energy-release-rate evaluation for delamination growth prediction in a multi-plate model of a laminate composite

    In this paper, numerical methods for the evaluation of the energy-release-rate along a delamination periphery under conditions of local buckling of the delaminate, as well as global buckling of the entire lami...

    B. P. Naganarayana, S. N. Atluri in Computational Mechanics (1995)

  18. No Access

    Article

    An analysis of an explicit algorithm and the radial return algorithm, and a proposed modification, in finite plasticity

    This paper presents an analysis of Nemat-Nasser's (1991) explicit algorithm and a radial return algorithm for isotropic Von Mises materials undergoing large deformations. It is found that the final-radial retu...

    L. H. Wang, S. N. Atluri in Computational Mechanics (1994)

  19. No Access

    Article

    Analysis of strain localization in strain-softening hyperelastic materials, using assumed stress hybrid elements

    Newly developed assumed stress finite elements, based on a mixed variational principle which includes unsymmetric stress, rotation (drilling degrees of freedom), pressure, and displacement as variables, are pr...

    W. Seki, S. N. Atluri in Computational Mechanics (1994)

  20. No Access

    Article

    A methodology for computing nonlinear fracture parameters for a bulging crack in a pressurised aircraft fuselage

    A computational methodology for obtaining nonlinear fracture parameters which account for the effects of plasticity at the tips of a bulging crack in a pressurised aircraft fuselage is developed. The methodolo...

    V. B. Shenoy, D. O. Potyondy, S. N. Atluri in Computational Mechanics (1994)

Page of 4