2019
DOI: 10.1177/1081286519856061
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Refined dimensional reduction for isotropic elastic Cosserat shells with initial curvature

Abstract: Using a geometrically motivated 8-parameter ansatz through the thickness, we reduce a three-dimensional shell-like geometrically nonlinear Cosserat material to a fully two-dimensional shell model. Curvature effects are fully taken into account. For elastic isotropic Cosserat materials, the integration through the thickness can be performed analytically and a generalized plane stress condition allows for a closed-form expression of the thickness stretch and the nonsymmetric shift of the midsurface in bending. W… Show more

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Cited by 20 publications
(49 citation statements)
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“…To compare our results with other six-parameter shell models, we write the strain energy density in an alternative useful form (equation (113)). We pay special attention to the comparison with the Cosserat shell model of order O ( h 5 ) , which has been presented recently in Bîrsan et al [12]. Although the derivation methods are different, we obtain the same form of the strain energy density, except for the coefficients of the transverse shear energy, which are unequal.…”
Section: Introductionmentioning
confidence: 91%
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“…To compare our results with other six-parameter shell models, we write the strain energy density in an alternative useful form (equation (113)). We pay special attention to the comparison with the Cosserat shell model of order O ( h 5 ) , which has been presented recently in Bîrsan et al [12]. Although the derivation methods are different, we obtain the same form of the strain energy density, except for the coefficients of the transverse shear energy, which are unequal.…”
Section: Introductionmentioning
confidence: 91%
“…where ε α β is the two-dimensional alternator ε 12 = ε 21 = 1 , ε 11 = ε 22 = 0 ) and a ( x 1 , x 2 ) determines the elemental area of the surface ω ξ In view of equations (1) and (13), we can show that (see f. (46) in Bîrsan et al [12])…”
Section: Introductionmentioning
confidence: 98%
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“…where E e := Q T e Grad s m − a is the elastic shell strain tensor , K e := Q T e axl Q e,α Q T e ⊗ a α is the elastic shell bending-curvature tensor, and we denote a α = y 0,α , a = Grad s y 0 , b = −Grad s n 0 , c = −n 0 × a [2,3,1].…”
mentioning
confidence: 99%