Jtam.dvi JOURNAL OF THEORETICAL AND APPLIED MECHANICS 46, 4, pp. 763-775, Warsaw 2008 RESPONSE OF BEAM ON VISCO-ELASTIC FOUNDATION TO MOVING DISTRIBUTED LOAD Roman Bogacz Cracow University of Technology and IPPT, Polish Academy of Sciences, Warsaw, Poland e-mail: rbogacz@ippt.gov.pl Włodzimierz Czyczuła Cracow University of Technology, Poland The paper is devoted to the study of several cases of stationary dyna- mical problems in which motion is driven by a distributed load acting on a beam on an elastic foundation at a moving position. The velocity of motion is assumed constant. In particular, cases of a load described by the Heaviside function (or its linear superposition) and a harmonic function are studied. Some problems examined by the authors in their previous investigations are reviewed. Key words: dynamics, travelling load, wave propagation 1. Introduction Thedevelopment of various kinds ofmodern technology, like explosive bonding of layered materials or tracked high-speed transportation systems, becomes more and more important. This makes a strong need for simplified but relia- blemodels of continuous orhybrid systems in order to studyvariousdynamical effects which influence durability of structures, damage of the environment or comfort of transportation.Thefirst studyof beamson theWinkler foundation subjected to a simple concentrated force moving with a constant speed was initiated by Timoshenko (1926). The first stationary solution to a simple sta- tionary case of theBernoulli-Euler beamonan elastic foundationwas properly obtained by Ludwig (1938). The case of a moving and oscillating force was formulated and partly solved byMathews (1958). The first proper solution to theMathews problemwas given byBogacz andKrzyżyński (1986). There are 764 R. Bogacz, W. Czyczuła various extensions of this classic problem towards more complicated but also more realistic models of structures and loads. A great deal of new effects were recognized by Bogacz et al. (1998) who examined the problem of an oscilla- ting loadmoving along aperiodic (variable in space) structure.Thedynamical effects for two or three-dimensional problems with moving loads have impor- tant practical engineering applications (Bogacz and Frischmuth, 2008). Some problems connected with a system of plates subjected to a traveling load can be found in Bogacz (2008), Bogacz and Frischmuth (2008). An application of the beammodel to the railway track mechanics is connected with taking into account the axial force into the model (Kerr, 1972). The aim of this paper is devoted to systematization and explanation of some new effects related to the moving distributed and oscillating load. 2. Beam on the Winkler foundation subjected to a uniformly distributed load acting on a segment The problem of vibration of a flexibly supported beamwith the stiffness EI, linearmass density mA, damping coefficient h andWinkler coefficient c, sub- jected to the distributed loadmovingwith the velocity V0, can be composed of the solution obtained for the limiting case of a load described by the following Heaviside function F0H(x−V0t) EIw,xxxx+Tw,xx+mAw,tt+hw,t+ cw=F0H(x−V0t) (2.1) A similar case of thebeam(without the compression force, T =0)was studied by Bogacz and Rozenbajgier (1979). The beam on an elastic foundation was generalized there to the case of a beam on a visco-elastic semi-space. The boundary conditions, equivalent to the condition of radiation, in the visco- elastic case take the following form limw(x) =      0 for x→∞ c F0 for x→−∞ (2.2) and in themoving coordinate system X =x−V0t (2.3) where thedisplacement w(X) aswell as itsderivatives w,X,w,XX, and w,XXX are continuous at X =0. Response of beam on visco-elastic foundation... 765 The equation of beam motion in the moving system of coordinates (2.3) takes the form EIw,XXXX +Tw,XX +mA(w,tt−2V0w,Xt+V 20w,XX)+ (2.4) +h(w,t−V0w,X)+ cw=F0H(X) In the stationary case, a characteristic equation ofEq. (2.4) takes the following form R4+4(Vq)2R2−8Vbq3R+4q4 =0 (2.5) where V = V0 Vcr Vcr = √ √ √ √ √ 4cEI mA − T mA q= √ c 4EI b= h 2 √ cmA Roots of Eq. (2.5) are R1 =S1+iD1 R2 =S1− iD1 R3 =S2+iD2 R4 =S2− iD2 S1 =−S2 (2.6) Using boundary conditions (2.2), the continuity conditions at X =0, one can obtain the following kind of solution before and behind the front of the load: — for X < 0 W1(X)= F0 c +exp(nX) { A1 sin [( 2V 2+n2− 2Vh n ) X ] + (2.7) +A2cos [( 2V 2+n2− 2Vh n ) X ]} — for X > 0 W2(X)= exp(−nX) { A3 sin [( 2V 2+n2+ 2Vh n ) X ] + (2.8) +A4cos [( 2V 2+n2+ 2Vh n ) X ]} where n is the positive root of the equation n6+2V 2n4+(V 4−1)n2−V 2b2 =0 (2.9) 766 R. Bogacz, W. Czyczuła and A1 =− F0 2Kc n 2V 2+n2− 2Vh n [ 2V 2(V 2+n2)−3 (Vh n )2 − Vh n (V 2+3n2) ] A2 =− F0 2Kc [ 2n2(V 2+n2)+ (Vh n )2 + Vh n (V 2+3n2) ] (2.10) A3 =− F0 2Kc n 2V 2+n2+ 2Vh n [ 2V 2(V 2+n2)−3 (Vh n )2 + Vh n (V 2+3n2) ] A4 =− F0 2Kc [ −2n2(V 2+n2)− (Vh n )2 + Vh n (V 2+3n2) ] K =2n2(V 2+n2)− (Vh n )2 The solution for the purely elastic case can be obtained from Eqs. (2.7) and (2.8) for h → 0. The solution has a different form for the sub-critical and super-critical case. The solution for the sub-critical case (V < 1) behind the front of the load W1(X) and before the front W2(X) is described by following formulas W1(X)= F0 2c [ 2− exp( √ 1−V 2X) ][ V 2√ 1−V 4 sin( √ 1+V 2X)+cos( √ 1+V 2X) ] (2.11) W2(X)=− F0 2c exp( √ 1−V 2X) [ V 2√ 1−V 4 sin( √ 1+V 2X)− cos( √ 1+V 2X) ] For the super-critical case (V > 1) the displacements are as follows W1(X)= F0 2c [ 2− ( 1+ V 2√ V 4−1 ) cos[( √ 1+V 2− √ V 2−1)X] ] (2.12) W2(X)=− F0 2c [( −1+ V 2√ V 4−1 ) cos[( √ 1+V 2+ √ V 2−1)X] ] It is visible that in the stationary elastic case, for a super-critical velocity of loadmotion V >Vcr, thewaves before andbehind the front of the load donot decay for |X| → ∞. Shorter waves with the phase velocity smaller than the group velocity propagate before the front of the load, and longer waves with the phase speed higher than the group velocity propagate behind the front of the load. The displacements in the sub-critical case are shown in Fig.2. In the linear case, superposition of the obtained solution for the Heviside function allows one to obtain various kinds of piece-wise constant loads distri- buted on a finite-length segment. For example, if we describe a load with a Response of beam on visco-elastic foundation... 767 Fig. 1.Wave velocity V0 versus wave number k for the Bernoulli-Euler beam on the Winkler foundation subjected to longitudinal force T Fig. 2. Displacements of the Bernoulli-Euler beam on theWinkler foundation in the sub-critical case (V =0.8) for various damping coefficients given value F1 distributed between x = 0 and x = L at t = 0, it is then possible to write the load as follows F(x,t)=F1[H(x−V0t)−H(x−L−V0t)] (2.13) In such a case, the solution must fulfill conditions (2.2) and, additionally, the continuity of displacements and derivatives w,X,w,XX, and w,XXX at X =0 and X =L. Let us now consider a more complicated model of the beam on an elastic foundation which takes into account shear deformation and rotary inertia of the cross-section – theTimoshenkobeam.Thecase of theTimoshenkobeamon an elastic foundation subjected touniformlydistributedmoving loadshasbeen studied by several authors (Fryba, 1972; Bogacz et al., 1989). The equation of motion of the Timoshenko beam takes the following form 768 R. Bogacz, W. Czyczuła EIϕ,xx+k ′AG(w,,x−ϕ)−mAIϕ,tt =0 (2.14) k′AG(w,xx−ϕ,x)−mAw,tt−hw,t− cw=−F0H(x−V0t) where ϕ is thebeamrotation due to pure shear, k′ – shear coefficient, G–mo- dulus of shear elasticity, A – cross-sectional area, and h – damping coefficient. Thefirst stationary solution obtained for the case of theTimoshenkobeam on an elastic foundation was obtained by Achenbach and Sun (1965). The shape of displacement in this solution is shown in Fig.3. Fig. 3. Displacements of the Timoshenko beam on theWinkler foundation for various values of the load speed. The results are found for a parameter range similiar to that used by Achenbach and Sun (1965) The solution obtained by Achenbach and Sun (1965) is qualitatively dif- ferent from that shown in Fig.4. Looking for the limiting stationary case, the set of equations (2.14) can be reduced to the following fourth-order equation with respect to displacement W(X) = w(X) √ A/I, where I is the moment of inertia of the cross-section Q(V 2)WIV +2Vh(V 2−V 2E)W ′′′+[V 2(V 2E +1)−V 2G]W ′′+ (2.15) +2VV 2EhW ′+V 2GW =F[V 2 GH(X)+(V 2−V 2E)H′′(X)] where F =F0 ( A Ic2 ) Q(V 2)= (V 2−V 2G)(V 2−V 2E) V 2E = EA2 Ic V 2G = k′GA2 Ic Response of beam on visco-elastic foundation... 769 Fig. 4. Displacements of the Bernoulli-Euler beam on theWinkler foundation in the super-critical case (V =1.2) for various damping coefficients Making use of the above equation, we can determine the discontinuity values of the derivatives of W(X) and rotation at the point X = 0. The solution to the problem consists in determination of displacements W(X) and rotation that satisfy equations (2.15). We shall obtain them by applying the Fourier transformation to the equations of motion. To investigate the effect of the load speed on the qualitative character of the solutions for the elastic system, i.e. h→ 0, let us consider two sets of parameters. Case I V 2E >V 2 G(V 2 G+1) (2.16) In this case, there exist threemain ranges of the load speed inwhich there are three corresponding different solutions like those obtained by Achenbach and Sun (1965) and shown in Fig.3. Within range No. 1, for |V | < V1, the solutions tend to the asymptotes W = 0 and W = 1 in monotonous ways. Within range No. 2 for V1 < V < V2, the solution vanishes monotonously before the load front and oscillates periodically around the value W = 1 behind the load front. Within range No. 3 for V > V2, the displacement and rotation before the load front are equal to zero, and behind the load the solution consists of superposition of two particular periodic solutions. This solution, unobservable in Fig.3, can be seen in Fig.6. 770 R. Bogacz, W. Czyczuła Fig. 5. Phase velocity Vf versus wave number k for two qualitatively different cases of the solution Case II V 2E V1 has a similar feature as in case I. The solution shown in Fig.6 for V 2 =15 illustrates qualitative behaviour of the beam in this region. The above case shows that there exists a set of parameters for the Ti- moshenko beam which can be taken qualitatively as the limiting case, i.e. transition to the Bernoulli- Euler beam. The change between case I and ca- se II is connectedwith the change from the hyperbolic to parabolic type of the equation. This is the reasonwhy the solution obtained byAchenbach and Sun (1965) is valid in thewhole range of velocity, but only for the set of parameters fulfilling inequality (2.16). Response of beam on visco-elastic foundation... 771 Fig. 6. Displacements of the Timoshenko beam on theWinkler foundation for various values of the load speed, in the case of parameters V 2E