Abstract
This contribution provides a semi-analytical model for the assessment of the three-dimensional stress field in thick, cylindrically curved cross-ply laminated shells subjected to different kinds of mechanical loadings under consideration of the free-edge effect. The model superimposes a closed-form analytical solution with a layerwise approach and the governing equations as well as the boundary conditions are derived by means of the minimum total potential energy principle utilizing the general Euler-Lagrange equations. Numerical results for thick cross-ply laminated shells undergoing uniform edge loadings and sinusoidal outer pressure are presented and the accuracy is verified by comparisons with full-scale, three-dimensional finite element computations. Those reveal an excellent agreement between the highly efficient semi-analytical model and the finite element approach for the free-edge stress fields in cross-ply laminated shells.
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References
. Kant T, Swaminathan K (2000) Estimation of transverse/interlaminar stresses in laminated composites – a selective review and survey of current developments. Composite Structures 49(1):65–75
Mittelstedt C, Becker W (2007) Free-edge effects in composite laminates. Applied Mechanics Reviews 60(5):217–245
Mittelstedt C, Becker W, Kappel A, Kharghani N (2022) Free-edge effects in composite laminates—a review of recent developments 2005–2020. Applied Mechanics Reviews 74(1):010,801
Srinivas S (1974) Analysis of laminated, composite, circular cylindrical shells with general boundary conditions. Nasa tr r-412, Langley Research Center, Hampton, Va. 23665
Ren JG (1987) Exact solutions for laminated cylindrical shells in cylindrical bending. Composites Science and Technology 29(3):169–187
Lekhnitskii SG (1963) Theory of elasticity of an anisotropic elastic body. Holden-Day series in mathematical physics, Holden-Day, San Francisco, CA
Lekhnitskii SG (1968) Anisotropic plates. Gordon and Breach, London, UK
Ko WL, Jackson RH (1989) Multilayer theory for delamination analysis of a composite curved bar subjected to end forces and end moments. Technical memorandum no. 4139, NASA Research Center, Edwards, CA, USA
Varadan TK, Bhaskar K (1991) Bending of laminated orthotropic cylindrical shells—an elasticity approach. Composite Structures 17(2):141–156
Miri AK, Nosier A (2011) Interlaminar stresses in antisymmetric angle-ply cylindrical shell panels. Composite Structures 93(2):419–429
Miri AK, Nosier A (2011) Out-of-plane stresses in composite shell panels: layerwise and elasticity solutions. Acta Mechanica 220(1-4):15–32
Nosier A, Miri AK (2010) Boundary-layer hygrothermal stresses in laminated, composite, circular, cylindrical shell panels. Archive of Applied Mechanics 80(4):413–440
Tahani M, Andakhshideh A, Maleki S (2016) Interlaminar stresses in thick cylindrical shell with arbitrary laminations and boundary conditions under transverse loads. Composites Part B: Engineering 98:151–165
Schnabel JE, Yousfi M, Mittelstedt C (2017) Free-edge stress fields in cylindrically curved symmetric and unsymmetric cross-ply laminates under bending load. Composite Structures 180:862–875
Kappel A, Mittelstedt C (2020) Free-edge stress fields in cylindrically curved cross-ply laminated shells. Composites Part B: Engineering 183:107,693
Kappel A, Mittelstedt C (2021) Interlaminar stress fields in circular cylindrical cross-ply laminated shells subjected to transverse loadings. International Journal of Solids and Structures 228:111,096
Ahmadi I (2019) Free edge stress prediction in thick laminated cylindrical shell panel subjected to bending moment. Applied Mathematical Modelling 65:507–525
Ahmadi I (2020) A three-dimensional formulation for levy-type transversely loaded cross-ply shell panels. International Journal of Mechanical Sciences 167:105,224
Kappel A, Dillen S, Mittelstedt C (2021) Hygrothermomechanical analysis of the free-edge stress fields in cylindrical cross-ply laminated shells. Mechanics of Advanced Materials and Structures 30(4):1–18
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Kappel, A., Mittelstedt, C. (2024). On the Semi-analytical Modelling of the Free-Edge Stress Field in Cross-Ply Laminated Shells Under Mechanical Loads. In: Altenbach, H., Hohe, J., Mittelstedt, C. (eds) Progress in Structural Mechanics. Advanced Structured Materials, vol 199. Springer, Cham. https://doi.org/10.1007/978-3-031-45554-4_6
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DOI: https://doi.org/10.1007/978-3-031-45554-4_6
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