Bistable prestressed shell structures

By E. Kebadze, Simon D. Guest, Sérgio Roberto Matiello Pellegrino. 2004

255 citations recorded by the source corpus.

Subfields: Civil and Structural Engineering, Mechanical Engineering, Mechanics of Materials

View Paper: https://www.semanticscholar.org/paper/4602a31baf5cf47baa35c61675600f85e888ae93

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In Civil and Structural Engineering

In Mechanical Engineering

In Mechanics of Materials

Citations in the corpus

On the thermally induced bistability of composite cylindrical shells for morphing structures (2012, background): “In the recent past, the multistability of slender laminates has received significant attention, because it has shown potential for morphing applications (e.g. Dano and Hyer, 1998; Seffen, 2007; Kebadze et al., 2004; Diaconu et al., 2008; Mattioni et al., 2009).”
On zero stiffness (2014, background): “The bistability can be achieved by imposing a state of prestress in the shell by an initial plastic forming process.(26) Using a simple inextensional shell deformation model,(27) a particular prestress state for the shell was found where the twisting deformation requires no external energy, see Figu”
Analytical models for bistable cylindrical shells (2006, methodology): “An alternative technique for making these structures bistable, by setting up an initial state of self-stress in the shell, is described by Kebadze et al. (2004) .”
Bistable plates for morphing structures: A refined analytical approach with high-order polynomials (2010, background): “In the recent past, the subject has received significant attention because multistable slender panels have shown potential for morphing applications (e.g. Dano and Hyer, 1998; Seffen, 2007; Kebadze et al., 2004).”
Buckling-induced smart applications: recent advances and trends (2015, unknown): “structure [42, 100, 104] [98, 111, 119, 121] [101, 102] [106] [28] [113, 116] [26] [156] [81, 157, 158] [124, 159, 160]”
Tristability of thin orthotropic shells with uniform initial curvature (2008, methodology): “where c2 (1 ; 0)[ (0; +1) is one of the principal curvatures and 2 [0; ). This expression for the curvature of inexensible shells reduces to the coordinate system used by Kebadze et al. (2004) and Guest and Pellegrino (2006) for the special case of cylindrical shells, for which G0 = 0. For c2 = G0”