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Showing 1 to 8 of 8 for “"laminated composite beams"”.

  1. Compression of thick laminated composite beams with initial impact-like damage

    While the study of compression after impact of laminated composites has been under consideration for many years. the complexity of the damage initiated by low velocity impact has not lent itself to simple predictive models for compression strength. The damage modes due to non-penetrating. low …

    vt Repository record for Compression of thick laminated composite beams with initial impact-like damage (opens in a new tab)

  2. Dynamic analysis and buckling of variable thickness laminated composite beams using conventional and advanced finite element formulations

    The behavior of variable thickness laminated composite beams has not so far been fully understood. In the present thesis, a finite element formulation is established for uniform and variable thickness composite beams (externally and mid-plane tapered composite beams). First the conventional …

    concordia Repository record for Dynamic analysis and buckling of variable thickness laminated composite beams using conventional and advanced finite element formulations (opens in a new tab)

  3. Nonlinear Finite Element Analysis of Laminated Composite Beams Subjected to Harmonic Excitations Using a 20 DOF Beam Element

    … the nonlinear analysis of antisymmetrically laminated composite beams including shear deformation subjected to harmonic excitation, using a 20-degree of freedom finite element beam. The beam has 10 degrees of freedom at each node: The axial displacements, the transverse deflection due to …

    embry-riddle Repository record for Nonlinear Finite Element Analysis of Laminated Composite Beams Subjected to Harmonic Excitations Using a 20 DOF Beam Element (opens in a new tab)

  4. Thermal Bending, Buckling and Post-Buckling Analysis of Unsymmetrically Laminated Composite Beams with the Effects of Moisture and Geometric Imperfections

    … buckling, and post-buckling of unsymmetrically laminated composite beams with imperfection under hygrothermal effects. Three different boundary conditions will be considered on this study. The non-linear governing partial differential equations are derived by taking into account the von-Karman …

    embry-riddle Repository record for Thermal Bending, Buckling and Post-Buckling Analysis of Unsymmetrically Laminated Composite Beams with the Effects of Moisture and Geometric Imperfections (opens in a new tab)

  5. A twenty DOF element for nonlinear analysis of unsymmetrically laminated beams

    … analysis of symmetrically and unsymmetrically laminated composite beams including shear deformation. There is a need for a simple and efficient method for analyzing unsymmetrically laminated beams since no other study on this topic is currently available. The beam element has ten degrees of p …

    vt Repository record for A twenty DOF element for nonlinear analysis of unsymmetrically laminated beams (opens in a new tab)

  6. Numerical Modeling and Analysis of Composite Beam Structures Subjected to Torsional Loading

    … theoretical solution for the torsion problem of laminated composites. He adopted the traditional formulation of the torsion problem based on Saint Venant's torsion theory. The eigenfunction expansion method was employed to solve the formulated problem. The analytical method is proposed in this …

    vt Repository record for Numerical Modeling and Analysis of Composite Beam Structures Subjected to Torsional Loading (opens in a new tab)

  7. Nonlinear static and transient analysis of generally laminated beams

    … and bend-twist couplings inherent to generally laminated composite beams. Further, a coupling between the shear deformation and the twisting is introduced. The lateral strains are assumed nonzero and retained in the formulation. The first model termed SVHSDT also accounts for the continuity of …

    vt Repository record for Nonlinear static and transient analysis of generally laminated beams (opens in a new tab)

  8. Dynamic response of thin-walled composite structures with application to aircraft wings

    … then the dynamic characteristics of thin-walled composite structures with the presence of bending torsion coupling. The dynamic response theory incorporates the dynamic stiffness matrix approach and generalised coordinates using the normal mode method. Structural components considered are …

    city-london Repository record for Dynamic response of thin-walled composite structures with application to aircraft wings (opens in a new tab)