1961
DOI: 10.1061/jmcea3.0000267
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Bending and Stretching of Laminated Aeolotropic Plates

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Cited by 54 publications
(7 citation statements)
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“…This acceptance shows the simple fundamental equations and ignores transverse normal and shear strain deformation of 2D elastic structure. Reissner and Stavsky, 83 Stavsky, 84 Dong et al, 85 Yang et al, 86 Ambartsumyan, 87 Whitney and Leissa, 88 Reddy, 39 and Whitney 89 have considered a simple 2D method of elastic structure theory for laminated composite thin structure.…”
Section: Laminate Theoriesmentioning
confidence: 99%
“…This acceptance shows the simple fundamental equations and ignores transverse normal and shear strain deformation of 2D elastic structure. Reissner and Stavsky, 83 Stavsky, 84 Dong et al, 85 Yang et al, 86 Ambartsumyan, 87 Whitney and Leissa, 88 Reddy, 39 and Whitney 89 have considered a simple 2D method of elastic structure theory for laminated composite thin structure.…”
Section: Laminate Theoriesmentioning
confidence: 99%
“…Table 1 shows some results for the vertical displacement at the center of the plate and the stresses in some characteristic points, for dierent side length/thickness ratios (a/h). In order to show the accuracy of the results, they are compared with the solution obtained by Stavsky [18] by means of the Classical Theory of Laminated Plates (CLPT) which is based on Kirchho's hypothesis. Note the dierence of the results when the thickness increases.…”
Section: Simply Supported Square Laminated Platementioning
confidence: 99%
“…The classical laminated plate theory (CLPT) is an extension of Love-Kirchhoff's classical plate theory for isotropic plates applied for thin laminates. This theory omitted the transverse shear deformation and rotary inertia effects [4][5][6]. To defeat the constraints of CLPT, Reissner [7] first developed the shear deformation theory with the effect of transverse shear deformation and rotary inertia.…”
Section: Introductionmentioning
confidence: 99%