810 YING LI AND CHANG-JUN CHENG ui(x1, t), <strong>vol</strong>ume fraction ϕ(xi, t) <strong>and</strong> temperature θ(xi, t) make the following functional arrive at the stationary value �(ui, ϕ, θ) = � t 0 (T + W + D − U) dt + �B, (19) where H = T + W + D − U is a generalized Hamilton function. Applying a variational calculation to (19) (whose detailed formulas are given in the Appendix) <strong>and</strong> substituting the results obtained into the variational equation <strong>of</strong> (19), that is, δ� = 0, then integrating (19) with regard to time from 0 to the final time t, <strong>and</strong> observing the beam has the appointed motions at the initial <strong>and</strong> final time, as well as the arbitrariness <strong>of</strong> the variables δui, δMϕ, δMθ on the interval [0, l], we obtain the differential equations <strong>of</strong> motion in terms <strong>of</strong> ui, Mϕ, Mθ, in which the balance <strong>of</strong> entropy has been differentiated relative to t1: � � D0hb u1,1 + (u2,1) 2 +(u3,1) 2 �� D0hb u1,1 + (u2,1) 2 +(u3,1) 2 2 �� D0hb 2 u1,1 + (u2,1) 2 + (u3,1) 2 2 + q1 = ρhbü1, ,1 � u2,1 � − D0Izu2,1111 ,1 + Iz Iy + Iz � � u3,1 − D0Iyu3,1111 ,1 (bv Mϕ − β Mθ),11 + q2 − N0u2,11 = ρhbü2 − ρ Izü2,11, + Iy (bv Mϕ − β Mθ),11 + q3 − N0u3,11 = ρhbü3 − ρ Iyü3,11, Iy + Iz αv Mϕ,11 + bv(Izu2,11 + Iyu3,11) − ξv Mϕ + qϕ + mv Mθ = ρχ ¨Mϕ, K Mθ,11 + βT0(Iz ˙u2,11 + Iy ˙u3,11) − mvT0 ˙Mϕ + qθ = ρce ˙Mθ. This is a set <strong>of</strong> coupled nonlinear equations for ui, Mϕ <strong>and</strong> Mθ, in which the effects <strong>of</strong> the axial forces N0, the neutral layer inertia ρhbü1, <strong>and</strong> the rotation inertias ρ Izü2,11 <strong>and</strong> ρ Iyü3,11 are included. It can be also seen that the boundary conditions at the end designated forces may be derived from the boundary virtual work equation in the variational equation δ� = 0. If we only consider a clamped-beam without axial forces, the boundary conditions at the ends (x1 = 0, l) are (20) ui = 0, u2,1 = 0, u3,1 = 0, Mϕ,1 = 0, Mθ = 0. (21) Observing that formula (18) is included in (19), the initial conditions at the initial time are given as ui = u 0 i , Mϕ = M 0 ϕ , Mθ = M 0 θ , ˙ui = ˙u 0 i , ˙Mϕ = ˙M 0 ϕ , (22) in which u 0 i , M0 ϕ , M0 θ , ˙u0 i , ˙M 0 ϕ are the known functions <strong>of</strong> x1. Especially, if the beam is at rest at the initial time, these functions are equal to zeros. 4. Solution method As application <strong>of</strong> the mathematical model above, the nonlinear mechanical characteristics <strong>of</strong> a two end fixed beam without the axial force are investigated, <strong>and</strong> the influences <strong>of</strong> parameters are considered. For
A NONLINEAR MODEL OF THERMOELASTIC BEAMS WITH VOIDS, WITH APPLICATIONS 811 convenience, we here study the plane bending <strong>of</strong> the beam only, that is, u2(x1, t) ≡ 0. As it is difficult to obtain the solution <strong>of</strong> the problem directly, we will apply the differential quadrature method (DQM) to discretize the nonlinear system on the spatial domain. The DQM is a numerical technique for solving boundary-valued problems. It was developed in [Bellman <strong>and</strong> Casti 1971], <strong>and</strong> since then it has been successfully employed to solve all kinds <strong>of</strong> problems in engineering <strong>and</strong> science due to the DQM owns the advantages <strong>of</strong> little amount <strong>of</strong> nodes <strong>and</strong> computation, high precision <strong>and</strong> good convergence <strong>and</strong> so on. The DQM approximates the derivative <strong>of</strong> a function, with respect to the independent variable at a given discrete point, as a weighted linear sum <strong>of</strong> the values <strong>of</strong> the function at all the discrete points chosen in the solution domain <strong>of</strong> the independent variable, in which the weighting coefficients are only associated with the given discrete points in the solution domain <strong>and</strong> independent <strong>of</strong> a certain problem. Therefore, any differential equations can be transformed into a set <strong>of</strong> the corresponding algebraic equations. Introduce the nondimensional variables <strong>and</strong> parameters a1 = bv D0 X = x1 h u1 u3 , U = , W = h , a2 = βT0 , a3 = D0 a9 = mv , a10 = ρce bvh 2 αv ¯h 2ρceV1 h , β1 = h , l V1 τ = t , l Mϕ ψ = 12 , h2 Mθ � = 12 , T0h 2 (23) , ξvh 2 mvT0h 2 a4 = , a5 = , αv αv � � V1 2 a6 = , a8 = V3 β , a11 = , ρce ρceV1h q3 , ¯p = , K D0 � D0 V1 = ρ , V3 � αv = . ρχ (24) From (24), one sees that the coefficients a1 <strong>and</strong> a3 are the coupling deformation-void parameters, which represent the coupling degree <strong>of</strong> the deformation <strong>and</strong> <strong>vol</strong>ume fraction field. The coefficient a6 is the ratio <strong>of</strong> the longitudinal wave velocity to the <strong>vol</strong>ume fraction wave velocity, which represents the ratio <strong>of</strong> the elastic constant to the void constant. The coefficient a4 is a void parameter. The coefficients a2 <strong>and</strong> a8 are the coupling deformation-heat parameters, which represent the coupling degree <strong>of</strong> the deformation <strong>and</strong> temperature field. The coefficient a10 is a convection heat transfer parameter, <strong>and</strong> a11 is the ratio <strong>of</strong> dilational wave velocity to thermal conductive coefficient. The coefficients a5 <strong>and</strong> a9 are the coupling void-heat parameters, which represent the coupling degree <strong>of</strong> the <strong>vol</strong>ume fraction <strong>and</strong> temperature field. The differential quadrature discretization forms <strong>of</strong> the nondimensional differential equations are N� A (2) k=1 β1 � N� k=1 N� l=1 A (1) ik Wk · N� ik Uk + β1 k=1 l=1 A (2) ik Uk · N� A (1) il Wl + N� N� A (2) k=1 β1 − β2 1 ik ψk + a3 k=1 N� a11 k=1 A (2) ik �k + a8β 2 1 k=1 A (2) il Wl = Üi, A (1) ik Uk · N� N� A 12 k=1 (4) ik Wk + a1 N� 12 k=1 N� A (2) ik Wk − a4 + 12 N� k=1 A (2) ik β 2 1 l=1 A (2) il Wl � + 3 2 β2 � N� 1 A k=1 (1) ik Wk �2 N� A l=1 (2) il Wl A (2) ik ψk − a2 12 ψi + a5 β2 1 ˙Wk − a9 ˙ψi − N� k=1 �i = a6 ¨ψi, � a10 + 1 � 12 a11 A (2) ik �k + ¯p β 2 1 β1 θ+ − θ− T0 = ¨Wi − β2 1 12 = ˙�i, N� k=1 A (2) ik ¨Wk, (25)
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