Based on the first-order shear deformation theory,a 3-node co-rotational triangular finite element formulation is developed for large deformation modeling of non-smooth,folded and multi-shell laminated composite struc...Based on the first-order shear deformation theory,a 3-node co-rotational triangular finite element formulation is developed for large deformation modeling of non-smooth,folded and multi-shell laminated composite structures.The two smaller components of the mid-surface normal vector of shell at a node are defined as nodal rotational variables in the co-rotational local coordinate system.In the global coordinate system,two smaller components of one vector,together with the smallest or second smallest component of another vector,of an orthogonal triad at a node on a non-smooth intersection of plates and/or shells are defined as rotational variables,whereas the two smaller components of the mid-surface normal vector at a node on the smooth part of the plate or shell(away from non-smooth intersections)are defined as rotational variables.All these vectorial rotational variables can be updated in an additive manner during an incremental solution procedure,and thus improve the computational efficiency in the nonlinear solution of these composite shell structures.Due to the commutativity of all nodal variables in calculating of the second derivatives of the local nodal variables with respect to global nodal variables,and the second derivatives of the strain energy functional with respect to local nodal variables,symmetric tangent stiffness matrices in local and global coordinate systems are obtained.To overcome shear locking,the assumed transverse shear strains obtained from the line-integration approach are employed.The reliability and computational accuracy of the present 3-node triangular shell finite element are verified through modeling two patch tests,several smooth and non-smooth laminated composite shells undergoing large displacements and large rotations.展开更多
针对边界元法中几乎奇异积分计算难题,本文提出一种基于6节点三角形等参数单元的三维高阶单元半解析算法.通过对三维声场基本解中的三角函数进行T a y l o r级数展开,分离出基本解中的奇异积分项.根据单元的几何特性,构造出与奇异积分...针对边界元法中几乎奇异积分计算难题,本文提出一种基于6节点三角形等参数单元的三维高阶单元半解析算法.通过对三维声场基本解中的三角函数进行T a y l o r级数展开,分离出基本解中的奇异积分项.根据单元的几何特性,构造出与奇异积分核函数具有相同奇异性的近似奇异核函数,对奇异积分项应用扣除法,将奇异积分核函数分为规则核函数和近似奇异核函数两项.规则核函数积分无奇异性,应用常规G a u s s数值积分就能够准确计算;近似奇异核函数积分由导出的半解析公式计算,即在局部极坐标系ρθ下分离积分变量,导出对变量ρ积分的解析计算列式,应用常规G a u s s数值积分计算变量θ积分,从而建立一种三维声场边界元法几乎奇异积分的半解析算法.算例结果表明,本文高阶单元半解析算法比双线性元算法更加有效且算法稳定,能够有效、准确地计算距离单元非常近的近边界点处的声压.展开更多
基金This work was supported by National Natural Science Foundation of China under Grant 11672266.
文摘Based on the first-order shear deformation theory,a 3-node co-rotational triangular finite element formulation is developed for large deformation modeling of non-smooth,folded and multi-shell laminated composite structures.The two smaller components of the mid-surface normal vector of shell at a node are defined as nodal rotational variables in the co-rotational local coordinate system.In the global coordinate system,two smaller components of one vector,together with the smallest or second smallest component of another vector,of an orthogonal triad at a node on a non-smooth intersection of plates and/or shells are defined as rotational variables,whereas the two smaller components of the mid-surface normal vector at a node on the smooth part of the plate or shell(away from non-smooth intersections)are defined as rotational variables.All these vectorial rotational variables can be updated in an additive manner during an incremental solution procedure,and thus improve the computational efficiency in the nonlinear solution of these composite shell structures.Due to the commutativity of all nodal variables in calculating of the second derivatives of the local nodal variables with respect to global nodal variables,and the second derivatives of the strain energy functional with respect to local nodal variables,symmetric tangent stiffness matrices in local and global coordinate systems are obtained.To overcome shear locking,the assumed transverse shear strains obtained from the line-integration approach are employed.The reliability and computational accuracy of the present 3-node triangular shell finite element are verified through modeling two patch tests,several smooth and non-smooth laminated composite shells undergoing large displacements and large rotations.
文摘针对边界元法中几乎奇异积分计算难题,本文提出一种基于6节点三角形等参数单元的三维高阶单元半解析算法.通过对三维声场基本解中的三角函数进行T a y l o r级数展开,分离出基本解中的奇异积分项.根据单元的几何特性,构造出与奇异积分核函数具有相同奇异性的近似奇异核函数,对奇异积分项应用扣除法,将奇异积分核函数分为规则核函数和近似奇异核函数两项.规则核函数积分无奇异性,应用常规G a u s s数值积分就能够准确计算;近似奇异核函数积分由导出的半解析公式计算,即在局部极坐标系ρθ下分离积分变量,导出对变量ρ积分的解析计算列式,应用常规G a u s s数值积分计算变量θ积分,从而建立一种三维声场边界元法几乎奇异积分的半解析算法.算例结果表明,本文高阶单元半解析算法比双线性元算法更加有效且算法稳定,能够有效、准确地计算距离单元非常近的近边界点处的声压.
