Mechanics of Composite Materials--nonlinear Effects: Presented at the 1st Joint Mechanics Meeting of ASME, ASCE, SES, MEET'N '93, Charlottesville, Virginia, June 6-9, 1993M. W. Hyer |
Contents
Flange Buckling and Postbuckling Response in Fiber Composite IBeams | 1 |
Mode Interaction in FRP Columns | 9 |
Interlaminar Stress Concentration in Postbuckled OpenSection Stiffeners | 19 |
Copyright | |
31 other sections not shown
Common terms and phrases
AMD-Vol applied axial behavior boundary conditions buckling load buckling mode chemical potential circumferential clamped coefficients components composite laminate Composite Materials computational configuration constitutive equations crack tip creep curvature curve cutout cylinder Cylindrical Shells damage deflection denote displacement edge Effects ASME 1993 elastic equations experimental failure fiber composite finite element analysis flange function global HT-MMC hydrostatic Hyer imperfection in-plane incremental initial interface isotropic kpsi laminated composite layer wave linear longitudinal material nonlinearity material properties matrix cracking maximum Mechanics of Composite Metal Matrix Composites METCAN method micromechanics mode shape modulus Newton's method nonlinear analysis Nonlinear Effects ASME obtained out-of-plane deformation panel parameters plies Poisson's ratio postbuckling response predicted pressure quasi-isotropic ratio shear strain shear stress shown in Figure simply supported solution specimen stiffeners stiffness stress-strain temperature tensile tensor tested tested tested thermal thickness thin unit cell values variables viscoelastic viscoplastic wavy