Pages that link to "Item:Q1822552"
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The following pages link to A consistent refined theory for flexure of a symmetric laminate (Q1822552):
Displaying 7 items.
- Predictor-corrector procedures for stress and free vibration analyses of multilayered composite plates and shells (Q807231) (← links)
- Postbuckling analysis of stiffened laminated composite panels, using a higher-order shear deformation theory (Q1196503) (← links)
- On bending-tension coupling of laminates (Q1610652) (← links)
- A single variable refined theory for free vibrations of a plate using inertia related terms in displacements (Q1658671) (← links)
- New approach for the analysis of flexure of symmetric laminates (Q3987103) (← links)
- A Layer-Wise Laminate Theory Rationally Deduced From the Three-Dimenstonal Elasticity (Q4393192) (← links)
- Stress analyses of laminates under cylindrical bending (Q5438229) (← links)