Pages that link to "Item:Q1210011"
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The following pages link to An improved plate theory of \(\{1,2\}\)-order for thick composite laminates (Q1210011):
Displaying 14 items.
- Computational homogenisation of composite plates: consideration of the thickness change with a modified projection strategy (Q316608) (← links)
- Refined zigzag theory for homogeneous, laminated composite, and sandwich beams derived from Reissner's mixed variational principle (Q904819) (← links)
- A high-order laminated plate theory with improved in-plane responses (Q1081377) (← links)
- Corrected 2D-theories for composite plates (Q1341915) (← links)
- Further results concerning the refined theory of anisotropic laminated composite plates (Q1342212) (← links)
- A method for improving the stress analysis performance of one- and two-dimensional theories for laminated composites (Q1384736) (← links)
- Complete stress field in sandwich panels with a new triangular finite element of single-layer theory (Q2495603) (← links)
- Finite element linear and nonlinear, static and dynamic analysis of structural elements: A bibliography (1992-1995) (Q2721478) (← links)
- A critical evaluation of two Reissner-Mindlin type models for composite laminated plates (Q2853555) (← links)
- Robust \(C^{0}\) high-order plate finite element for thin to very thick structures: mechanical and thermo-mechanical analysis (Q2895053) (← links)
- A homogeneous limit methodology and refinements of computationally efficient zigzag theory for homogeneous, laminated composite, and sandwich plates (Q3068795) (← links)
- (Q4223449) (← links)
- An accurate determination of stresses in thick laminates using a generalized plate theory (Q5202350) (← links)
- Analysis of thick sandwich construction by a \(\{3,2\}\)-order theory. (Q5946072) (← links)