Composite methods for structural dynamics

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Composite methods are an approach applied in structural dynamics and related fields. They combine various methods in each time step, in order to acquire the advantages of different methods. The existing composite methods show satisfactory accuracy and powerful numerical dissipation, which is particularly useful for solving stiff problems[1] and differential-algebraic equations.[2]

Definitions

After spatial discretization, structural dynamics problems are generally described by the second-order ordinary differential equation: Mu¨+Cu˙+f(u,t)=R(t). Here u, u˙ and u¨ denote the displacement, velocity and acceleration vectors respectively, M is the mass matrix, C is the damping matrix, f(u,t) collects the internal force, and R(t) is the external load. At the initial time t0, the initial displacement and velocity are supposed to be given as u0 and u˙0, respectively, and the initial acceleration can be solved as u¨0=M1(R(t0)Cu˙0f(u0,t0)). For numerical analysis, the overall time domain [t0,tN] is divided into a series of time steps by t1, t2, , tk, tk+1, . Taking the step [tk,tk+1] (tk+1tk=h is the step size), the main concept of composite methods is to subdivide the current step to several sub-steps [tk,tk+γ1], [tk+γ1,tk+γ2], , and to use different numerical methods in each sub-step. Although there are lots of available methods, see the review,[3] the existing composite methods basically employ the combination of the trapezoidal rule and linear multistep methods. However, to acquire at least second-order accuracy and unconditional stability, the scalar parameters of each method and the division of sub-steps need to be determined carefully.

Two examples of composite method

Two-sub-step Bathe method

The Bathe method [4][5] is a two-sub-step method. In the first sub-step [tk,tk+γ] (tk+γtk=γh, γ(0,1)), the trapezoidal rule is used as: uk+γ=uk+γh2(u˙k+u˙k+γ) u˙k+γ=u˙k+γh2(u¨k+u¨k+γ) Mu¨k+γ+Cu˙k+γ+f(uk+γ,tk+γ)=R(tk+γ) In the second sub-step [tk+γ,tk+1] (tk+1tk+γ=(1γ)h), the 3-point Euler backward method is employed as u˙k+1=1γγhuk1(1γ)γhuk+γ+2γ(1γ)huk+1 u¨k+1=1γγhu˙k1(1γ)γhu˙k+γ+2γ(1γ)hu˙k+1 Mu¨k+1+Cu˙k+1+f(uk+1,tk+1)=R(tk+1) For nonlinear dynamics, that is, the internal force f is a nonlinear function with respect to u, the Newton-Raphson iterations can be used to solve the nonlinear equations per step. The parameter γ is usually set as 12 and 22 in practice. The Bathe method is second-order accurate and unconditionally stable from linear analysis. Besides, this method can provide strong numerical dissipation for high-frequency content, which is helpful to damp out the stiff components and enhance the stability for nonlinear dynamics. On this basis, to acquire prescribed degree of numerical dissipation, the ρ-Bathe method [6] was developed by replacing the 3-point Euler backward method in the second sub-step with a general formula: uk+1=uk+h(q0u˙k+q1u˙k+γ+q2u˙k+1) u˙k+1=u˙k+h(q0u¨k+q1u¨k+γ+q2u¨k+1) Mu¨k+1+Cu˙k+1+f(uk+1,tk+1)=R(tk+1) The parameters are selected as recommended γ=22(1+ρ)1ρ if ρ[0,1);γ=12 if ρ=1 q1=ρ+12γ(ρ1)+4,q0=(γ1)q1+12,q2=γq1+12 With the set of parameters, the ρ-Bathe method can also achieve second-order accuracy and unconditional stability. Moreover, by adjusting the parameter ρ, this method can provide tunable degree of numerical dissipation. The method with a smaller ρ shows stronger numerical dissipation, but lower accuracy in the low-frequency content. When ρ=0, it is equivalent to the original Bathe method with γ=22.

Three-sub-step composite method

Following the idea of the Bathe method, the three-sub-step composite methods that use the trapezoidal rule in the first two sub-steps were also discussed.[7][8][9] They divides the current step into [tk,tk+γ1], [tk+γ1,tk+γ2] and [tk+γ2,tk+1], and generally, the first two sub-steps are set as equal size, that is γ2=2γ1. In the first two sub-steps, the trapezoidal rule is used, as uk+γ1=uk+γ1h2(u˙k+u˙k+γ1) u˙k+γ1=u˙k+γ1h2(u¨k+u¨k+γ1) Mu¨k+γ1+Cu˙k+γ1+f(uk+γ1,tk+γ1)=R(tk+γ1) and uk+γ2=uk+γ1+(γ2γ1)h2(u˙k+γ1+u˙k+γ2) u˙k+γ2=u˙k+γ1+(γ2γ1)h2(u¨k+γ1+u¨k+γ2) Mu¨k+γ2+Cu˙k+γ2+f(uk+γ2,tk+γ2)=R(tk+γ2) In the last sub-step, a general formula is utilized as uk+1=uk+h(c0u˙k+c1u˙k+γ1+c2u˙k+γ2+c3u˙k+1) u˙k+1=u˙k+h(c0u¨k+c1u¨k+γ1+c2u¨k+γ2+c3u¨k+1) Mu¨k+1+Cu˙k+1+f(uk+1,tk+1)=R(tk+1) For this method, Li et al.[8] offered two optimal set of parameters, as a=12(1±ρ),c0=(a+1)γ12+4γ114γ1,c1=1+(a1)γ12,c2=(1a)γ122γ1+14γ1,c3=γ12 Here γ2=2γ1 is assumed, and γ1 is the minimum value that satisfies 48(a1)γ1432(a5)γ13192γ12+96γ1160. The resulting two sub-families are all second-order accurate, unconditionally stable, and can provide tunable numerical dissipation by adjusting ρ. They become the same when ρ=0. When 0<ρ<1, the sub-family with a=12(1ρ) shows better amplitude and period accuracy than the ρ-Bathe method under the same computational costs, and the sub-family with a=12(1+ρ) further improves the period accuracy at the cost of lower amplitude accuracy.

Analysis

In structural dynamics, the test model for property analysis is the single degree-of-freedom homogeneous equation, as u¨+2ξωu˙+ω2u=0 Here ξ is the damping ratio and ω is the natural frequency. Applying the composite method to the test model yields the compact scheme Xk+1=AXk Here Xk={uk;u˙k;u¨k} and A is the amplitude matrix, which governs the properties of a method. Generally, A has one zero characteristic root and a pair of conjugate complex roots λ1,2, which can be solved from λ2A1λ+A2=0 Here A1 is the trace of A and A2 is the sum of second-order principal minors of A. They are functions of ξ, ωh, and the parameters of the method.

Accuracy

From the compact scheme, the difference equation only with respect to the displacement can be written as uk+1A1uk+A2uk1=0 The local truncation error σ is defined as σ=u(tk+1)A1u(tk)+A2u(tk1) The method is called sth-order accurate if σ=O(hs+1).

Stability

For physically stable systems (ξ0, ω0), the method can give stable solutions if the spectral radius ρ=max{|λ|}1. A method is called unconditionally stable if the condition ρ1 is satisfied for any h0, otherwise it is called conditionally stable. The spectral radius at the high-frequency limit, i.e. ωh+, is denoted as ρ, which is usually employed to indicate the degree of numerical dissipation, as used above.

Amplitude decay ratio and period elongation ratio

In addition to the accuracy order, the amplitude decay ratio and period elongation ratio are also usually evaluated to measure the amplitude and period accuracy in the low-frequency content. The exact solution of the test model is u(t)=eξωt(c1cosωdt+c2sinωdt),ωd=ω1ξ2 Here c1 and c2 are constants determined by the initial conditions. The numerical solution can be also expressed as a similar form, as uk=eξωtk(c1cosωdtk+c2sinωdtk),ωd=ω1ξ2 Likewise, c1 and c2 are also determined by the initial conditions and they should be close to c1 and c2 respectively for a convergent method. The damping ratio ξ and frequency ω can be obtained from the norm |λ| and phase λ, as[10] ξ=ln|λ|(λ)2+(ln|λ|)2,ω=(λ)2+(ln|λ|)2h Here ξ is called the amplitude decay ratio, and TTT (T=2πω,T=2πω) is called the period elongation ratio.

Example

File:Spectral radius of the Bathe method.tif File:Amplitude decay ratio of the Bathe method.tif File:Period elongation ratio of the Bathe method.tif Consider the Bathe method, A1 and A2 have the form as A1=2(γ44γ3+6γ24)ω2h2+8(γ2)2(γ2ω2h2+4)((γ1)2ω2h2+(γ2)2) A2=(γ44γ3+8γ28γ+4)ω2h2+4(γ2)2(γ2ω2h2+4)((γ1)2ω2h2+(γ2)2) Here the undamped case, i.e. ξ=0, is considered for simplicity. One can check that this method can satisfy the conditions of second-order accuracy and unconditional stability. With γ=12 and 22, the spectral radius, amplitude decay ratio, and period elongation ratio are shown here. It can be observed that this method can provide good amplitude and period accuracy in the low-frequency content, while strong numerical dissipation, as ρ=0, in the high-frequency content.

See also

References

  1. Hairer, Ernst; Wanner, Gerhard (1996). Solving ordinary differential equations (Second ed.). Berlin: Springer-Verlag. ISBN 978-3-540-60452-5.
  2. Kunkel, Peter; Mehrmann, Volker Ludwig (2006). Differential-algebraic equations : analysis and numerical solution. European Mathematical Society. ISBN 978-3-03719-017-3.
  3. Tamma, Kumar K.; Har, Jason; Zhou, Xiangmin; Shimada, Masao; Hoitink, Andrew (15 July 2011). "An Overview and Recent Advances in Vector and Scalar Formalisms: Space/Time Discretizations in Computational Dynamics—A Unified Approach". Archives of Computational Methods in Engineering. 18 (2): 119–283. doi:10.1007/s11831-011-9060-y. S2CID 61608667.
  4. Bathe, Klaus-Jürgen; Baig, Mirza M. Irfan (December 2005). "On a composite implicit time integration procedure for nonlinear dynamics". Computers & Structures. 83 (31–32): 2513–2524. doi:10.1016/j.compstruc.2005.08.001.
  5. Bathe, Klaus-Jürgen; Noh, Gunwoo (May 2012). "Insight into an implicit time integration scheme for structural dynamics". Computers & Structures. 98–99: 1–6. doi:10.1016/j.compstruc.2012.01.009.
  6. Noh, Gunwoo; Bathe, Klaus-Jürgen (February 2019). "The Bathe time integration method with controllable spectral radius: The ρ∞-Bathe method". Computers & Structures. 212: 299–310. doi:10.1016/j.compstruc.2018.11.001. S2CID 125901946.
  7. Chandra, Yenny; Zhou, Yang; Stanciulescu, Ilinca; Eason, Thomas; Spottswood, Stephen (11 April 2015). "A robust composite time integration scheme for snap-through problems". Computational Mechanics. 55 (5): 1041–1056. Bibcode:2015CompM..55.1041C. doi:10.1007/s00466-015-1152-3. hdl:1911/80759. S2CID 120256889.
  8. 8.0 8.1 Li, Jinze; Yu, Kaiping; Li, Xiangyang (26 April 2019). "A novel family of controllably dissipative composite integration algorithms for structural dynamic analysis". Nonlinear Dynamics. 96 (4): 2475–2507. doi:10.1007/s11071-019-04936-4. S2CID 150178628.
  9. Ji, Yi; Xing, Yufeng (April 2020). "An optimized three-sub-step composite time integration method with controllable numerical dissipation". Computers & Structures. 231: 106210. doi:10.1016/j.compstruc.2020.106210. S2CID 213806573.
  10. Zhou, X.; Tamma, K. K. (7 February 2004). "Design, analysis, and synthesis of generalized single step single solve and optimal algorithms for structural dynamics". International Journal for Numerical Methods in Engineering. 59 (5): 597–668. Bibcode:2004IJNME..59..597Z. doi:10.1002/nme.873. S2CID 120453750.