Jing et al., 2019 - Google Patents
Closed-form critical buckling load of simply supported orthotropic plates and verificationJing et al., 2019
- Document ID
- 8023753238823372178
- Author
- Jing Z
- Sun Q
- Liang K
- Chen J
- Publication year
- Publication venue
- International Journal of Structural Stability and Dynamics
External Links
Snippet
The buckling mode is important to determine the critical load of specially orthotropic rectangular plates under axial compression with simply supported boundary. However, in classical laminated plate theory (CLPT), the critical buckling mode can only be obtained by …
- 230000001808 coupling 0 abstract description 20
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Phan et al. | Analysis of laminated composite plates using a higher‐order shear deformation theory | |
Li et al. | Low-velocity impact response of sandwich plates with GRC face sheets and FG auxetic 3D lattice cores | |
Pingulkar et al. | Free vibration analysis of laminated composite plates using finite element method | |
Nemeth | Buckling and postbuckling behaviour of laminated composite plates with a cut-out | |
AZZI et al. | Strength of laminated composite materials. | |
Jing et al. | Closed-form critical buckling load of simply supported orthotropic plates and verification | |
Swaminathan et al. | Analytical solutions using a higher-order refined theory for the static analysis of antisymmetric angle-ply composite and sandwich plates | |
Abedi et al. | A new solution method for free vibration analysis of rectangular laminated composite plates with general stacking sequences and edge restraints | |
Sekine et al. | Buckling analysis of elliptically delaminated composite laminates with consideration of partial closure of delamination | |
Khare et al. | Higher-order closed-form solutions for thick laminated sandwich shells | |
Esmaeili et al. | Vibrations of graphene platelet reinforced composite doubly curved shells subjected to thermal shock | |
Zhang et al. | Three-dimensional meta-architecture with programmable mechanical properties | |
Biswal et al. | Dynamic stability of woven fiber laminated composite shallow shells in hygrothermal environment | |
Kant et al. | Estimation of interlaminar stresses in fibre reinforced composite cylindrical shells | |
Kumari | Dynamic response of composite panels under thermo-mechanical loading | |
Zenkour | Buckling and free vibration of elastic plates using simple and mixed shear deformation theories | |
Pradyumna et al. | Dynamic instability behavior of laminated hypar and conoid shells using a higher-order shear deformation theory | |
Chaudhuri et al. | Fourier solution to higher order theory based laminated shell boundary-value problem | |
Lal et al. | Probabilistic-based nonlinear progressive failure analysis of piezoelectric laminated composite shell panels in hygrothermal environment | |
Tan et al. | A simplified delamination modelling methodology for triaxial braided composites with macro-scale solid finite-element models | |
Dong et al. | A simple locking-alleviated 3D 8-Node mixed-collocation C0 finite element with overintegration, for functionally-graded and laminated thick-section plates and shells, with & without z-pins | |
Goldberg et al. | Incorporation of plasticity and damage into an orthotropic three-dimensional model with tabulated input suitable for use in composite impact problems | |
Liaw et al. | Reliability of uncertain laminated shells due to buckling and supersonic flutter | |
Lal et al. | Effect of random system properties on initial buckling of composite plates resting on elastic foundation | |
Hearley et al. | Micromechanics modeling of textiles for re-entry parachute applications |