Hyer et al., 1991 - Google Patents
The use of curvilinear fiber format to improve buckling resistance of composite plates with central circular holesHyer et al., 1991
- Document ID
- 5971153238573087545
- Author
- Hyer M
- Lee H
- Publication year
- Publication venue
- Composite structures
External Links
Snippet
This paper explores the gains in buckling performance that can be achieved by deviating from the conventional straightline fiber format and considering the situation whereby the fiber orientation in a layer, or a group of layers, can vary from point to point in the plane of …
- 239000000835 fiber 0 title abstract description 133
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Hyer et al. | The use of curvilinear fiber format to improve buckling resistance of composite plates with central circular holes | |
| Owen et al. | Anisotropic elasto‐plastic finite element analysis of thick and thin plates and shells | |
| CA1106735A (en) | Three-dimensional, multi-directional structure | |
| Gaudenzi et al. | Multi‐layer higher‐order finite elements for the analysis of free‐edge stresses in composite laminates | |
| Duan et al. | A two-step optimization scheme based on equivalent stiffness parameters for forcing convexity of fiber winding angle in composite frames | |
| Adali | Multiobjective design of an antisymmetric angle-ply laminate by nonlinear programming | |
| Mazaev et al. | Static bending strength of sandwich composite plates with tetrachiral honeycombs | |
| Kant | Dynamics of laminated composite plates with a higher order theory and finite element discretization | |
| Roy et al. | Three-dimensional effective moduli of orthotropic and symmetric laminates | |
| Liang et al. | Optimum design of fiber-reinforced composite cylindrical skirts for solid rocket cases subjected to buckling and overstressing constraints | |
| Kaveh et al. | Optimal design of laminated composite structures via hybrid charged system search and particle swarm optimization | |
| Abouhamzeh et al. | Buckling optimisation of sandwich cylindrical panels | |
| Kam et al. | Optimum design of laminated composite foam-filled sandwich plates subjected to strength constraint | |
| Maharudra et al. | Effect of trapezoidal shapes on the thermal buckling behaviour of perforated composite plates | |
| Lee et al. | The Use of Curvilinear Fiber Format to Improve Buckling Resistance of Plates with Central Circular Holes1 | |
| Hyer et al. | Innovative design of composite structures: the use of curvilinear fiber format to improve buckling resistance of composite plates with central circular holes | |
| Ding et al. | Optimal design of laminated plate for minimizing frequency response based on discrete material model and mode reduction method | |
| Tabaddor | Mechanical properties of cord-rubber composites | |
| Xue et al. | Optimization of thermal buckling control for composite laminates with PFRC actuators using trigonometric shear deformation theory | |
| Taylor et al. | Damping characteristics of laminated thick plates | |
| Ovesy et al. | Buckling analysis of laminated composite plates using higher order Semi—Analytical finite strip method | |
| Zou et al. | Buckling analysis of composite laminates under end shortening by higher‐order shear deformable finite strips | |
| Maksimović | Optimum design of composite structures | |
| BERT et al. | Analysis of thick rectangular plates laminated of bimodulus composite materials | |
| Crouzet-Pascal | Buckling analysis of laminated composite plates |