Consider a 2-dof system whose matrix equation of motion is given as
[m1100m22](x¨1x¨2) +[k11k21k12k22](x1x2)=(00), (i)
where m11=m,m22=mr2,k11=k1+k2,k12=k21=k2L2−k1L1,k22=k2L22+k1L12,x1=x is the
translational displacement, and x2 = θ is the angular or rotational displacement.
If m = 4000 kg, k1=k2=20,000N/m,r=0.8m,m22=mr2=2560kgm2,L1=1.4m,andL2=0.9 m, find the natural frequencies and normal modes of the 2-dof system.
a. Since the system is undamped and therefore the responses have no delay or phase difference with respect to the applied force, one can write
(x2x1)=(X2X1)cosωt=(ΘX)cosωt.
In this equation, X and Θ are the amplitudes of instantaneous displacements xi.
Substituting the above solution and its derivatives into Equation (i) and upon simplification, one has
[(k11−m11ω2)k21k12(k22−m22ω2)](ΘX)=(00) (ii)
or writing it in a more concise form
[Z(ω)](X2X1)=(00)
where the so-called impedance matrix has been defined by Equation (4.18) as
[(k11–m1ω2)k21k12(k22–m2ω2)](X2X1)=(0F1) (4.18)
[Z(ω)]=[(k11–m11ω2)k21k12(k22–m22ω2)]
The frequency equation is
∣∣∣∣∣(k11−m11ω2)k21k12(k22−m22ω2)∣∣∣∣∣=0.
Substituting the system parameters given above and writing λ = ω²,
∣∣∣∣∣40,000–4000λ10,00010,00055,400−2560λ∣∣∣∣∣=0.
Operating on this equation, one has
(40,000−4000λ)(55,400−2560λ)−(10,000)2=0.
This quadratic equation in λ gives λ1=9.2173,λ2=59.8457, so that the two natural frequencies are
ω1=9.2173=3.036rad/s, (iia)
ω2=59.8457=4.736srad (iib)
In order to obtain the mode shapes, one first substitutes ω1 into Equation (ii), resulting in
(ΘX)(1)=−3.18m/rad (iva)
where the subscript (1) on the lhs of the equation denotes the amplitude ratio associated with the first natural frequency.
Similarly, substituting ω2 into Equation (ii), one has
(ΘX)(2)=0.202m/rad. (ivb)
Equations (iva) and (ivb) give the two mode shapes of the 2-dof system.