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1 Dr. Peter Avitabile Modal Analysis & Controls Laboratory 22.457 Mechanical Vibrations - Chapter 4 Mechanical Vibrations Chapter 4 Peter Avitabile Mechanical Engineering Department University of Massachusetts Lowell

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Page 1: Mechanical Vibrations Chapter 4 - Faculty Server Contactfaculty.uml.edu/pavitabile/22.457/ME22457_Chapter4_021703_MACL.pdf · 22.457 Mechanical Vibrations - Chapter 4 Mechanical

1 Dr. Peter AvitabileModal Analysis & Controls Laboratory22.457 Mechanical Vibrations - Chapter 4

Mechanical VibrationsChapter 4

Peter AvitabileMechanical Engineering DepartmentUniversity of Massachusetts Lowell

Page 2: Mechanical Vibrations Chapter 4 - Faculty Server Contactfaculty.uml.edu/pavitabile/22.457/ME22457_Chapter4_021703_MACL.pdf · 22.457 Mechanical Vibrations - Chapter 4 Mechanical

2 Dr. Peter AvitabileModal Analysis & Controls Laboratory22.457 Mechanical Vibrations - Chapter 4

Impulse Excitation

Impulsive excitations are generallyconsidered to be a large magnitudeforce that acts over a very shortduration timeThe time integral of the force is

When the force is equal to unity and the timeapproaches zero then the unit impulse exists andthe delta function has the property of

(4.1.1)∫= dt)t(FF̂

( ) ξ≠=ξ−δ tfor0t

Page 3: Mechanical Vibrations Chapter 4 - Faculty Server Contactfaculty.uml.edu/pavitabile/22.457/ME22457_Chapter4_021703_MACL.pdf · 22.457 Mechanical Vibrations - Chapter 4 Mechanical

3 Dr. Peter AvitabileModal Analysis & Controls Laboratory22.457 Mechanical Vibrations - Chapter 4

Impulse Excitation

Integrated over all time, the delta function is

If this function is multiplied times any forcingfunction then the product will result in only onevalue at t=ξ and zero elsewhere

(4.1.2)∫∞

∞<ξ<=ξ−δ0

01dt)t(

∫∞

∞<ξ<ξ=ξ−δ0

0)(fdt)t()t(f (4.1.3)

Page 4: Mechanical Vibrations Chapter 4 - Faculty Server Contactfaculty.uml.edu/pavitabile/22.457/ME22457_Chapter4_021703_MACL.pdf · 22.457 Mechanical Vibrations - Chapter 4 Mechanical

4 Dr. Peter AvitabileModal Analysis & Controls Laboratory22.457 Mechanical Vibrations - Chapter 4

Impulse Excitation

Considering impact-momentum on the system, asudden change in velocity is equal to the actualapplied input divided by the force.Recall that the free response due to initialconditions is given by

tcos)0(xtsin)0(xx nnn

ω+ωω

= &

Page 5: Mechanical Vibrations Chapter 4 - Faculty Server Contactfaculty.uml.edu/pavitabile/22.457/ME22457_Chapter4_021703_MACL.pdf · 22.457 Mechanical Vibrations - Chapter 4 Mechanical

5 Dr. Peter AvitabileModal Analysis & Controls Laboratory22.457 Mechanical Vibrations - Chapter 4

Impulse Excitation

Then the velocity initial condition yields

and it can be seen that the solution includes h(t)

(4.1.4)

(4.1.5)

)t(hF̂tsinm

F̂x nn

=ωω

=

tsinm

1)t(h nn

ωω

=

Page 6: Mechanical Vibrations Chapter 4 - Faculty Server Contactfaculty.uml.edu/pavitabile/22.457/ME22457_Chapter4_021703_MACL.pdf · 22.457 Mechanical Vibrations - Chapter 4 Mechanical

6 Dr. Peter AvitabileModal Analysis & Controls Laboratory22.457 Mechanical Vibrations - Chapter 4

Impulse Excitation

When damping is considered in the solution, thefree response is given as (x(0)=0)

which can be written as

or as

(4.16)

tsine)0(xt1sin1e)0(xx d

d

t2

n2n

tn

ωω

=ζ−ωζ−ω

=σ−ζω− &&

t1sine1m

F̂x 2n

t2

n

n ζ−ωζ−ω

= ζω−

)t(hF̂tsinem

F̂x dt

d=ω

ω= σ−

Page 7: Mechanical Vibrations Chapter 4 - Faculty Server Contactfaculty.uml.edu/pavitabile/22.457/ME22457_Chapter4_021703_MACL.pdf · 22.457 Mechanical Vibrations - Chapter 4 Mechanical

7 Dr. Peter AvitabileModal Analysis & Controls Laboratory22.457 Mechanical Vibrations - Chapter 4

Arbitrary Excitation

Using the unitimpulse responsefunction, theresponse due toarbitrary loadingscan be determined.The arbitrary forceis considered to bea series of impulses

Page 8: Mechanical Vibrations Chapter 4 - Faculty Server Contactfaculty.uml.edu/pavitabile/22.457/ME22457_Chapter4_021703_MACL.pdf · 22.457 Mechanical Vibrations - Chapter 4 Mechanical

8 Dr. Peter AvitabileModal Analysis & Controls Laboratory22.457 Mechanical Vibrations - Chapter 4

Arbitrary Excitation

Since the system is considered linear, then thesuperposition of the responses of each individualimpulse can be obtained through numericalintegration

This is called the superposition integral. But it isalso referred to as the

Convolution Integralor

Duhammel’s Integral

(4.2.1)∫ ξξ−ξ=t

0

d)t(h)(f)t(x

Page 9: Mechanical Vibrations Chapter 4 - Faculty Server Contactfaculty.uml.edu/pavitabile/22.457/ME22457_Chapter4_021703_MACL.pdf · 22.457 Mechanical Vibrations - Chapter 4 Mechanical

9 Dr. Peter AvitabileModal Analysis & Controls Laboratory22.457 Mechanical Vibrations - Chapter 4

Step Excitation

Determine the indamped response due to a step.For the undamped system,

which is substituted into (4.2.1) to give

(4.2.2)

tsinm

1)t(h nn

ωω

=

( ) ξξ−ωω

= ∫ dtsinm

F)t(xt

0n

n

0

( )tcos1kF)t(x n

0 ω−=

Page 10: Mechanical Vibrations Chapter 4 - Faculty Server Contactfaculty.uml.edu/pavitabile/22.457/ME22457_Chapter4_021703_MACL.pdf · 22.457 Mechanical Vibrations - Chapter 4 Mechanical

10 Dr. Peter AvitabileModal Analysis & Controls Laboratory22.457 Mechanical Vibrations - Chapter 4

Step Excitation

This implies that the peak response is twice thestatical displacement

(4.2.2)( )tcos1kF)t(x n

0 ω−=

0 5 10 15 20 25 300

0.2

0.4

0.6

0.8

1

1.2

1.4

1.6

1.8

2

Time

Dis

plac

emen

t

Dis placement vers us Time

Note: Force selected such that F/k ratio is 1.0

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11 Dr. Peter AvitabileModal Analysis & Controls Laboratory22.457 Mechanical Vibrations - Chapter 4

Step Excitation

When damping is included in the equation, then

and

(4.2.2)t1sin

1me)t(h 2

n2n

tn

ζ−ωζ−ω

=ζω−

ψ−ζ−ω

ζ−ω−=

ζω−t1cos

1me1

kF)t(x 2

n2n

t0

n

(4.2.3)

Page 12: Mechanical Vibrations Chapter 4 - Faculty Server Contactfaculty.uml.edu/pavitabile/22.457/ME22457_Chapter4_021703_MACL.pdf · 22.457 Mechanical Vibrations - Chapter 4 Mechanical

12 Dr. Peter AvitabileModal Analysis & Controls Laboratory22.457 Mechanical Vibrations - Chapter 4

Step Excitation

This can be simplified as

tsinme)t(h d

d

ω=

σ−

ψ−ω

ω−=

σ−tcos

me1

kF)t(x d

d

t0

M=1 ; K=2

C=0

C=0.1

C=0.5C=1.0

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13 Dr. Peter AvitabileModal Analysis & Controls Laboratory22.457 Mechanical Vibrations - Chapter 4

Base Excitation

For base excitation,

the equation of motion is expressed as z=x-y andwill result in

Notice that the F/m term is replaced by thenegative of the base acceleration (ie, F=ma)

(3.5.1)

(4.2.4)yzz2z 2nn &&&&& −=ω+ζω+

)yx(c)yx(kxm &&&& −−−−=

yxz −= (3.5.2)

Page 14: Mechanical Vibrations Chapter 4 - Faculty Server Contactfaculty.uml.edu/pavitabile/22.457/ME22457_Chapter4_021703_MACL.pdf · 22.457 Mechanical Vibrations - Chapter 4 Mechanical

14 Dr. Peter AvitabileModal Analysis & Controls Laboratory22.457 Mechanical Vibrations - Chapter 4

Base Excitation

For and undamped systeminitially at rest, thesolution for the relativedisplacement is

(4.2.5)( ) ξξ−ωξω

−= ∫ dtsin)(y1)t(zt

0n

n&&

Page 15: Mechanical Vibrations Chapter 4 - Faculty Server Contactfaculty.uml.edu/pavitabile/22.457/ME22457_Chapter4_021703_MACL.pdf · 22.457 Mechanical Vibrations - Chapter 4 Mechanical

15 Dr. Peter AvitabileModal Analysis & Controls Laboratory22.457 Mechanical Vibrations - Chapter 4

Ramp Excitation and Rise Time

This solution must always be considered in twoparts - the time less than and greater than t1

The ramp of the force is

and h(t) for the convolution integral is

(4.4.1)

=

10 t

tF)t(f

(4.4.1)tsink

tsinm

1)t(h nn

nn

ωω

=ωω

=

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16 Dr. Peter AvitabileModal Analysis & Controls Laboratory22.457 Mechanical Vibrations - Chapter 4

Ramp Excitation and Rise Time

The response for the first part of the ramp is

and the response of the step portion after t1 is

(4.4.2)

11n

n

1

0

n

t

0 10

n

ttt

tsintt

kF

d)t(sint

Fk

)t(x

<

ωω

−=

ξξ−ωξω

= ∫

( )1

1n

1n

1

10 ttt

ttsint

ttkF)t(x >

ω

−ω−

−−=

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17 Dr. Peter AvitabileModal Analysis & Controls Laboratory22.457 Mechanical Vibrations - Chapter 4

Ramp Excitation and Rise Time

The superposition of the two pieces of the solutiongives the total response due to the force as

(4.4.3)( )

11n

1n

1n

n0 ttt

ttsint

tsin1kF)t(x >

ω

−ω+

ωω

−=

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18 Dr. Peter AvitabileModal Analysis & Controls Laboratory22.457 Mechanical Vibrations - Chapter 4

Rectangular Pulse

The rectangular pulse is the sum of two differentstep functions - one positive and one negativeshifted in time

Step Up

Step down

Combined

(4.4.4)( ) 1n0

tttcos1F

)t(kx<ω−=

(4.4.5)

(4.4.6)

( )( ) 11n0

ttttcos1F

)t(kx<−ω−−=

( )( ) ( )( ) 11nn0

ttttcos1tcos1F

)t(kx<−ω−−ω−=

( )( ) ( )( ) 11nn0

ttttcostcosF

)t(kx<−ω+ω−=

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19 Dr. Peter AvitabileModal Analysis & Controls Laboratory22.457 Mechanical Vibrations - Chapter 4

0 10 20 30 40 50 60 70 80 90 100-0.6

-0.4

-0.2

0

0.2

0.4

0.6

0.8

Time

Dis

plac

emen

t

Dis placement vers us Time

MATLAB Examples - VTB3_1VIBRATION TOOLBOX EXAMPLE 3_1

>> m=1; c=.1; k=2; tf=100; F0=1;>> vtb3_1(m,c,k,F0,tf)>>

Page 20: Mechanical Vibrations Chapter 4 - Faculty Server Contactfaculty.uml.edu/pavitabile/22.457/ME22457_Chapter4_021703_MACL.pdf · 22.457 Mechanical Vibrations - Chapter 4 Mechanical

20 Dr. Peter AvitabileModal Analysis & Controls Laboratory22.457 Mechanical Vibrations - Chapter 4

0 10 20 30 40 50 60 70 80 90 1000

0.5

1

Time

Dis

plac

emen

t

Dis placement vers us Time

MATLAB Examples - VTB3_2VIBRATION TOOLBOX EXAMPLE 3_2

>> m=1; c=.1; k=2; tf=100; F0=1;>> VTB3_2(m,c,k,F0,tf)>>>>

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21 Dr. Peter AvitabileModal Analysis & Controls Laboratory22.457 Mechanical Vibrations - Chapter 4

MATLAB Examples - VTB1_4VIBRATION TOOLBOX EXAMPLE 1_4 – pulse

>> clear; p=1:1:1000; pp=p./p; ppp=[(p./p-p./p) pp (p./p-p./p) (p./p-p./p)];>> x0=0; v0=0; m=1; d=.5; k=2; dt=.01; n=4000;>> u=ppp; [x,xd]=VTB1_4(n,dt,x0,v0,m,d,k,u);>> t=0:dt:n*dt; plot(t,x);plot(t,x);>>

0 5 10 15 20 25 30 35 40-0.4

-0.2

0

0.2

0.4

0.6

0.8

1

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22 Dr. Peter AvitabileModal Analysis & Controls Laboratory22.457 Mechanical Vibrations - Chapter 4

0 5 10 15 20 25 300

0.05

0.1

0.15

0.2

0.25

0.3

0.35

0.4

0.45

0.5

MATLAB Examples - VTB1_4VIBRATION TOOLBOX EXAMPLE 1_4 – ramp up (basically a static problem)

>> clear; x0=0; v0=0; m=1; d=.5; k=2; dt=.01; n=3000;>> t=0:dt*100:n; u=t./3000; [x,xd]=VTB1_4(n,dt,x0,v0,m,d,k,u);>> t=0:dt:n*dt; plot(t,x);>>