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Statistical models of elasticity in main chain and smectic liquid ...

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100 CHAPTER 4. THE ELASTICITY OF SMECTIC-A ELASTOMERSOn elim<strong>in</strong>ation the free energy density is given by{f = 1 2 µ 1+rλ 2 xz +λ2 +λ 2 zx + 1λ 2 zx +λ 2 + 2rλ xzλ zx√λλ 2 2 zx +λ 2+ λ2 zxr ( 1+λ 2 )}xzλ 2 . (4.79)This can be m<strong>in</strong>imized w.r.t λ xz <strong>and</strong> λ zx . The first <strong>of</strong> these yields the expressionλ zxλ xz = −√ (4.80)λ2 zx +λ2. On substitut<strong>in</strong>g this <strong>in</strong>to the expression obta<strong>in</strong>ed after m<strong>in</strong>imisation w.r.t λ zxwe obta<strong>in</strong> the follow<strong>in</strong>g equationλ 2 λ zx((−1+λ2zx +λ 2) √λ 2 zx +λ 2( 1+λ 2 zx +λ2) = 0. (4.81)From this equation it is clear that the follow<strong>in</strong>g real solutions for λ zx areobta<strong>in</strong>edλ zx = ± √ 1−λ 2 ,0 (4.82)The first <strong>of</strong> these solutions is only valid for λ < 1 <strong>and</strong> gives λ xz = −λ zx ,λ yy = 1, λ zz = λ. In this solution λ corresponds to a rotation about the yaxis. This solution is disregarded here <strong>and</strong> the second, λ zx = 0, is exam<strong>in</strong>ed.From this result it follows that the director does not rotate when a stretch <strong>in</strong>the plane <strong>of</strong> the layers is applied. The rema<strong>in</strong><strong>in</strong>g components <strong>in</strong> this case, <strong>and</strong>the free energy density are given byλ yy = 1 (4.83)λλ zz = 1 (4.84){f = 1 2 µ λ 2 + 1 }λ 2 +1 . (4.85)The Poisson ratios <strong>of</strong> the material <strong>in</strong> this configuration are <strong>of</strong> <strong>in</strong>terest experimentally.In this case the Poisson ratios are (1,0) <strong>in</strong> the (y,z) directionsrespectively. Note that s<strong>in</strong>ce the material is <strong>in</strong>compressible the sum <strong>of</strong> thePoisson ratios must be 1.Imposed λ xzFor an imposed λ xz , as shown <strong>in</strong> Fig. 4.9 c), it is not immediately clear howgeneral a deformation matrix is required. Initially an upper triangular deformationmatrix is considered here, <strong>and</strong> followed by a more general type <strong>of</strong>deformation matrix ⎛ ⎞λ xx 0 λλ = ⎝ 0 λ yy 0 ⎠. (4.86)0 0 λ zz

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