Article
Open Access
Exact geometry solid-shell element based on a sampling surfaces technique for 3D stress analysis of doubly-curved composite shells
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G. M. Kulikov
Published/Copyright:
November 30, 2015
Received: 2015-8-1
Accepted: 2015-9-16
Published Online: 2015-11-30
© 2015 G. M. Kulikov et al.
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Keywords for this article
Sampling surfaces method;
Doubly-curved
composite shell;
Hybrid-mixed four-node solid-shell element;
3D stress analysis
Creative Commons
BY-NC-ND 3.0
Articles in the same Issue
- Exact geometry solid-shell element based on a sampling surfaces technique for 3D stress analysis of doubly-curved composite shells
- Free vibrations and buckling analysis of laminated plates by oscillatory radial basis functions
- Relative performance of antisymmetric angle-ply laminated stiffened hypar shell roofs with cutout in terms of static behavior
- Probabilistic fracture investigation of symmetric angle ply laminated composite plates using displacement correlation method
- Numerical simulation of tests for the evaluation of the performance of the reinforced concrete slabs strengthening by FRCM
- On Asymptotic Theory of Beams, Plates and Shells
- Vibration analysis of FG cylindrical shells with power-law index using discrete singular convolution technique
- Influence of locational states of submicron fibers added into matrix on mechanical properties of plain-woven Carbon Fiber Composite
- Modelling of Piezothermoelastic Beam with Fractional Order Derivative
- Vibrations of Composite Laminated Circular Panels and Shells of Revolution with General Elastic Boundary Conditions via Fourier-Ritz Method
- Buckling optimisation of sandwich cylindrical panels
- Lateral-torsional buckling of compressed and highly variable cross section beams
- Open and closed shear-walls in high-rise structural systems: Static and dynamic analysis
- Characterization of ABS specimens produced via the 3D printing technology for drone structural components
- Experimental Study on Nonlinear Vibrations of Fixed-Fixed Curved Beams
- A multipurpose modular drone with adjustable arms produced via the FDM additive manufacturing process
- Material Distribution Optimization for the Shell Aircraft Composite Structure
- Geometric nonlinear free vibration of axially functionally graded non-uniform beams supported on elastic foundation
- The Influence of the Load Model and other Parameters on the Dynamic Behavior of Curved-in-Plane Bridges
- Free Vibration Study of Anti-Symmetric Angle-Ply Laminated Plates under Clamped Boundary Conditions