2022
DOI: 10.36959/422/459
|View full text |Cite
|
Sign up to set email alerts
|

Cylindrical Panel Like Response of Fully Surface Parallel Restrained Simply Supported Hyperbolic Paraboloidal Thick General Cross-ply Panels

Abstract: An analytical (exact in the limit) solution to the boundary-value problem of deformation of a finite-dimensional general cross-ply thick hyperbolic-paraboloidal panel, modeled using a third order shear deformation theory, is presented. Of special interest is the issue of cylindrical panel-like response, in the presence of full surface-parallel constraints at all four edges of a thick antisymmetric cross-ply panel of negative Gaussian curvature. Interaction of the membrane action due to negative Gaussian curvat… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1

Citation Types

0
4
0

Year Published

2022
2022
2022
2022

Publication Types

Select...
1

Relationship

1
0

Authors

Journals

citations
Cited by 1 publication
(4 citation statements)
references
References 111 publications
(209 reference statements)
0
4
0
Order By: Relevance
“…Recent decades have, following the pioneering lead by Basset [85], witnessed the introduction of second-and third-order shear deformation theories (TSDT), entailing continuity of quadratic and cubic, respectively, distribution, of the surface-parallel (in-plane for flat panels) displacement components through the laminate thickness [19], see for detailed reviews by Reddy [19], and Chaudhuri and Kabir [86] for the decades prior to 2000, and Giunta, et al [87], and Chaudhuri and Oktem [88,89], thereafter.…”
Section: Analytical or Strong Form Of Solutionsmentioning
confidence: 99%
See 3 more Smart Citations
“…Recent decades have, following the pioneering lead by Basset [85], witnessed the introduction of second-and third-order shear deformation theories (TSDT), entailing continuity of quadratic and cubic, respectively, distribution, of the surface-parallel (in-plane for flat panels) displacement components through the laminate thickness [19], see for detailed reviews by Reddy [19], and Chaudhuri and Kabir [86] for the decades prior to 2000, and Giunta, et al [87], and Chaudhuri and Oktem [88,89], thereafter.…”
Section: Analytical or Strong Form Of Solutionsmentioning
confidence: 99%
“…It has been noted earlier that for cross-ply laminates, while the former can only produce particular solutions for very specific set of boundary constraints [88], i.e. the SS3 prescribed at all four edges, the latter essentially solves a curved or straight beam type of boundary-value problems, because of the SS3 being prescribed at the remaining two opposite edges; see Appendix A for definition of various boundary constraints.Oktem and co-workers [88][89][99][100][101][102][103][104][105] presented boundary-discontinuous type double Fourier series solutions of highly coupled system of partial differential equations (relating to cross-ply laminated plates/shells) subjected to various boundary conditions. Needless to state, Navier [19,90,91] and Levy-type solutions [19,[92][93][94][95][96][97][98] to thick cross-ply flat and curved panels serve as special cases of the above.…”
Section: Analytical or Strong Form Of Solutionsmentioning
confidence: 99%
See 2 more Smart Citations