Strain rate and adhesive energy dependent viscoplastic damage modeling for nanoparticulate composites: Molecular dynamics and micromechanical simulations B.J. Yang1, H. Shin2, H. Kim2, H.K. Lee1,a) 1 Department of Civil and Environmental Engineering, Korea Advanced Institute of Science and Technology (KAIST), 291 Daehak-ro, Yuseong-gu, Daejeon 305-701, Republic of Korea 2 Graduate School of Energy Environment Water Sustainability (EEWS), Korea Advanced Institute of Science and Technology (KAIST), 291 Daehak-ro, Yuseong-gu, Daejeon 305-701, Republic of Korea a) Electronic mail: leeh@kaist.ac.kr Parameters U1 and U2 in Eq. (2). By carrying out the lengthy algebra, the parameters U1 and U 2 can be expressed as U1 2H 21 H1 31 21 , U2 2H2 1 (S.1) where 1 and m1 denote the Lame’s constants of NPs, and the components H1 and H2 are defined as follows: H1 2 2 1 1 1 2 2 , 1 2 2 1 31 2 2 H2 2 1 2 2 (S.2) 1 2S21 S1 31 21 , 2 2 S2 1 (S.3) M1 2S21 S1 31 21 1 , M 2 2 S2 11 (S.4) in which 1 2 with with 1 10 0 1 3S1 1 0 1 0 3 3S1 2 S 2 1 0 0 2 S2 1 0 0 1 0 1 2 2 S 2 1 0 0 (S.5) where q is the bulk modulus of q-phase (q=0, 1), and S1 and S2 are the parameters of Eshelby’s tensor with the interface effect which are given in Yang et al.8 VE Derivation process and results of the effective viscoelastic constitutive equation C* E First, the effective elasticity tensor C* for the NP-reinforced composites yields C*E *Eij kl *E ik jl il jk (S.6) with *E 0 31 2 2 33 2 4 1 20 1 3 1 (S.7) *E 20 2 4 2 Here, 0 and 0 denote Lame’s constants of the matrix, and L 2 q- 1 = {2b x q 2 q- 1 } + a q (1- 2x2 q ) f q (2x2q - 1)(3x2q- 1 + 2x2q - 1) , L 2q = b qf q , (q = 1, 2) (S.8) x2 q = 2S2b qf q , ( q = 1, 2) (S.9) 1- 2x2 q in which { } x2 q- 1 = f q 2S2a q + S1 (3a q + 2b q ) , where a 1 and b1 are listed in Eq. (S.5), and a 2 and b 2 are given in 2 S1 , 3S1 2S2 1 2S2 1 2 1 4S2 2 (S.10) Based on the superposition principle,6,15 the effective viscoelastic constitutive equation can be derived by combining the effective elasticity tensor and the Laplace transformation (LT). Hence, the effective elasticity tensor in the transformed domain (TD) CTD reads * TD TD CTD ik jl il jk * * ij kl * with (S.11) TD TD TD TD *TD 0TD 31TD 2TD 2 3 3 2 4 1 2 0 1 3 (S.12) 1 TD *TD 20TD TD 2 4 2 with L TD 2 q- 1 {2b = TD TD q 2 q- 1 x } + a qTD (1- 2x2TDq ) f q (2x2TDq - 1)(3x2TDq- 1 + 2x2TDq - 1) , L TD 2q = b qTDf q 1- 2x2TDq , (q = 1, 2) (S.13) with { } x2TDq- 1 = f q 2S2a qTD + S1 (3a qTD + 2b qTD ) , x2TDq = 2S2b qTDf q , (q = 1, 2) (S.14) in which TD 1 10TD 0TD 1 3S1 1 0TD 1 0TD 3 3S1 2 S2 1 0TD 0TD 2 S2 1 0TD 0TD 1TD 1 0TD 2 2S2 1 0TD 0TD 2TD S1 , 3S1 2S2 1 2S2 1 (S.15) 2TD 1 4S2 2 TD TD where the LT of the L𝑎́ me constants 0 and 0 are defined as 0TD 0 0 s , 0 s0 0TD 0 0 s 0 s0 (S.16) where 0 signify the viscosity of the matrix, and s denotes the Laplace constant. By taking the inverse Laplace transform of CTD * , the effective viscoelasticity tensor of the nanocomposites CVE * can be obtained by taking the direct inverse Laplace transform, or explicitly described as VE VE CVE ik jl il jk * * ij kl * in which (S.17) *VE t exp 0 0 2 S Z S 3S 2 3 3 1 4 5 6 2 1 2 1 4 *VE (S.18) t exp 0 0 7 0 2tZ1S 2 1 1 in which Z1t 0 2 , 0 Z10 2 S2 1 1 1 1 exp t 0 1 0 2 exp t 0 0 Z 2 2 S 2 1 1 3 exp 0 0 Z 2 2 S 2 1 1 1 3S1 2 S 2 1 1 4 6t 0 Z1S 2 3S1 2 S 2 1 1 Z 2 2 S 2 2 S 21 (S.19) 5 1 4 2 2 31 3 2 and Z1 1 2S2 1 1 , Z2 1 3S1 1 1 , Z3 1 2 1 (S.20) with t 0 1 , 0 1 exp 2 2 1 1 2 1 1 1 2 2 3 4Z3 2 S2 2 3 0 20 1 1 , t 0 1 1 1 2 0 4 2 1 2exp 5 21 2 11 3 2 2 2 21 51 3 2 (S.21) 6 6 1 3 5 1 6 2 2 2 2 1 41 3 7 6 2 0 1 1 3 0 2 2 31 1 1 2 2 8 3 0 2 2 12 2 1 5 , and 2 t 0 2 1 1 1 0 9 3exp t 2 201 3 0 exp 0 3 1 0 3 9S12 1 1 2011 3 S2 40 2 7 1 40 2 3 0 2 2 1 12 2 5 , 4 S2 40 2 1 4 9 2 2 8 , 6 2 01 23 1 , (S.22) 5 2 23 S2 2 405 3 0 6 1 1 7 4 Z3 2 S2 2 1 1 11 2 S2 2 where t signify the arbitrary time, which is defined as t t / . Here, denotes the strain rate. The fourth-rank tensor T in Eq. (10). The fourth-rank tensor T can be defined as T = T 1dij dkl + T 2 (dik d jl + dil d jk ) (S.23) with 2 T 1 = (3P1 + 2 P2 ) T 1 + 2 P1 (3P1 + 4 P2 )T 2 , T 2 = 4 P22T 2 (S.24) where the fourth-rank tensor Pijkl = P1dij dkl + P2 (dik d jl + dil d jk ) are P1 = - (c 1 + c 3 ) , (2c 2 + 2c 4 + 1)(3c 1 + 2c 2 + 3c 3 + 2c 4 + 1) P2 = 1 4c 2 + 4c 4 + 2 (S.25) in which c 2 q- 1 = f q {(1- 3S1 - 2S2 )a q - 2S1b q }, c 2 q = b qf q (1- 2S2 ), (S.26) (q=1, 2) Furthermore, the fourth-rank tensor Tijkl = T1dij dkl + T2 (dik d jl + dil d jk ) are f1 é 2 24m0 45 J12 P 12 + 60 J12 P 1P 2 - 4P 22 (P 3 - 5 J12 ) 5 êë f 1 T 2 = 1 (144m02 P 22P 3 )+ 5 2 T1 = }ùúû- { 1 3 (S.27) in which P1 = m0 - m1 k 0 - k1 + 6m0 {m0 + 2 (m1 - m0 )S2 } 9k 0 {k 0 (3S1 + 2S2 - 1)- 2k 1 (3S1 + 2S2 )} m0 - m1 P2= , 4m0 {m0 (2S2 - 1)- 2m1S2 } with 2 1 2 2 2 1 0 P 3 = J - 72 J1 J 2 + 15 J + 4 J n (7n0 - 10) (S.28) J1 = G(1 + n1 ) { } 3 (k + 2)(1- 2n1 )+ G(1 + n1 ) r s - G éê3G(7 + 5n1 )- 4 {k sr (1 + n 0 )+ msr (2n 0 - 1)+ 3}(10n1 - 7)ù ú ë û J2 = 3h11 (S.29) where G= m1 / m0 and n q is the Poisson’s ratio of q-phase. k sr , msr , and h11 are interface parameters, which are given in Yang et al.8