1995
DOI: 10.1016/0020-7683(94)00301-c
|View full text |Cite
|
Sign up to set email alerts
|

Stress concentration of finite composite laminates weakened by multiple elliptical holes

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
3
1

Citation Types

0
23
0

Year Published

2004
2004
2023
2023

Publication Types

Select...
6
2

Relationship

0
8

Authors

Journals

citations
Cited by 41 publications
(23 citation statements)
references
References 5 publications
0
23
0
Order By: Relevance
“…It was demonstrated by Muc, Ulatowska [62] and Xu Xiwu et al [63]. Tan [64] introduced the approximate formulas for the stress concentration factors for the orthotropic laminated plates valid in the range 0≤b/a≤1 -Eq. (29):…”
Section: Buckling Of Cylindrical Shells With Domed Headsmentioning
confidence: 99%
“…It was demonstrated by Muc, Ulatowska [62] and Xu Xiwu et al [63]. Tan [64] introduced the approximate formulas for the stress concentration factors for the orthotropic laminated plates valid in the range 0≤b/a≤1 -Eq. (29):…”
Section: Buckling Of Cylindrical Shells With Domed Headsmentioning
confidence: 99%
“…Xiwu et al [9,10] studied a finite composite plate weakened by elliptical holes under different in-plane loading, treated as an anisotropic multiple connected plates. Using the complex potential method in the plane theory of elasticity of an isotropic body, an analytical solution concerned with stress concentration around an elliptical hole or holes in finite composite fibrous plate is obtained.…”
Section: Introductionmentioning
confidence: 99%
“…More recent work on this problem using complex variables include papers by Ukadgaonker and Rao (2000), Xiwu et al (1995), Wu and Cheng (1999), Chen and Hsu (1996), Bryukhanova (1967), Wang and Hasebe (2000), Tsukrov and Novak (2002), Datsyshin and Marchenko (1985), Vigdergauz (1993), Exadaktylos et al (2003), Cherkaev and Grabovsky (1998). Ukadgaonker and Rao (2000) solved the bending problem for laminated composite plates with openings of different shapes and Xiwu et al (1995) considered a finite laminate with elliptical hole under in-plane extensional and shear loads.…”
Section: Introductionmentioning
confidence: 99%
“…Ukadgaonker and Rao (2000) solved the bending problem for laminated composite plates with openings of different shapes and Xiwu et al (1995) considered a finite laminate with elliptical hole under in-plane extensional and shear loads. Datsyshin and Marchenko (1985) solved for the stress concentration around curvilinear cracks in a half-plane problem by satisfying the boundary conditions numerically using Gauss quadrature formulas.…”
Section: Introductionmentioning
confidence: 99%