Question

A mass of 50kg is hung from a spring of stiffness ?=?.?×105 (?/? ) and damper ?=100 ?.?/? , which is attached to two aluminum beams with ?=71×109 (Pa), moment of inertia ?=?.?×10−? (??), and length of 255 (mm ). The beam is supported at its free end. Determine:
(a) Equivalent stiffness and equation of motion of the system.
(b) Damped natural frequency of the system (??) in (Hz).
(c) Free vibration response of the system in time domain,?(?), when ?(? )=10mm and ?̇(? )=100 mm/s.
(d) Simulation and plot of the response of system in MatLab/Simulink

255 mm Aluminum I= 3,5 x 10-8m+ 32.5 x 10 N/m 50 kg 100 N. s/m -

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Answer #1

a)

kA = stiffness of one aluminium beam in shown orientation = 3*E*I/L^3

= 3*71*3.5*10/0.255^3

= 449600.8323N/m

(here L= length of one aluminium beam)

The equivalent system can be shown as:

here,

k1 = spring stiffness = 2.5*10^5 N/m and

C = damping coefficient = 100N.s/m

The two springs with stiffness kA are in parallel and can be combined to get one spring (net stiffness = kA + kA) as shown:

Now, the springs with stiffness 2kA and k1 are in series with each other and can be combined to give one spring (of net stiffness 2kA *k1 ki + 2kA 2 * 449600.8323* 250000 = 195614.4192N/m = k) 250000 + 2 * 449600.8323 as shown below:

Therefore, equivalent stiffness of the system is, k = 195614.4192N/m ____________ eq.1

Consider the free body diagram as shown below:

к их та Сх

equation of motion for the system is:

n* 7 +*i k *I=0

__________________ Answer to part a

b)

Ccr = critical damping coefficient of the system = 2*(k*n)^(0.5)

= 2*(195614.4192*50)^(0.5)

= 6254.8288N.s/m

therefore, \xi = damping ratio = C/Ccr = 100/6254.8288 = 0.01599

since \xi < 1 => the system is under damped.

wn = natural frequency of the system = (k/n)^(0.5) = 62.5483rad/s,

therefore, wd = damped natural frequency of the system = wn*(1-\xi^2)^0.5 = 62.54030331rad/s

____________________________ Answer to part b

c)

free vibration response of such a system is given by:    A* e-*W* * sin(wd*t + o)

where, A and \phi are constants that can be found using boundary conditions.

applying boundary conditions:

i) at t=0s, x = 10mm,

=> A*sin(\phi) = 10 ____________________ eq. 2

ii) at t=0s, \dot{x} = 100mm/s and using A*sin(\phi) = 10 we get:

=> A*cos(\phi)*wd - 10*\xi*wn = 100

or A * cos(0)=- 100 + 10 * 0.01599 * 62.5483 62.54030331 = 1.75889 ______________ eq.3

performing (eq.2)^2 + (eq.3)^2 and using (sin(\phi))^2 + (cos(\phi))^2 = 1, we get:

or A = (1.75889) + 100

=> A= 10.15350649mm ____________ eq. 4

putting this in eq.2, we get:

\phi = 1.396688rad_________ eq.5

therefore, system response is:

(t) = 10.15350649 * e-1.0001473*+ * sin(62.54030331 *t + 1.396688) _________eq. 6

___________________ Answer to part c

d)

In MATLAB, the code is written as follows:

ou WN IIIIII t = 0:0.01:7; $7s analysis time x = 10.15350649*exp(-1.0001473*t).*sin (62.54030331*t + 1.396688); $displacement

Graph plotted for first 7s is as shown below:

displacement response curve of the system displacement response Wwwwwwwwwwww 1 2 3 5 67 4 time(s)

It can be seen that, the system nearly reaches equilibrium at t = 7s.

_________________ Answer to part d

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