Philadelphia University Faculty of Engineering Mechanical Engineering Department Dr. Adnan Dawood...

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Philadelphia University Faculty of Engineering

Mechanical Engineering Department

Dr. Adnan Dawood Mohammed(Professor of Mechanical Engineering)

Mechanical VibrationsForced Vibration of a Single Degree of Freedom System

Harmonically Excited Vibration

Physical system

force offrequency theis

force of amplitude theis cos

sin

:forms following theof one may takesIt force. harmonic a is

motion ofEquation ...

tjo

oo

o

eFtF

FtFtF

tFtF

tF

tFkxxcxm

Harmonically Excited Vibration

amplitude' response statesteadty ' thecalled is X , X(t)

as written becan solution The .frequency same with the

harmonic is (solution) response t theexpect thacan wefrequency with

harmaonic is n)(excitatio force theBecause equation. homogenuosnon

for thesolution theisIt :response state(steady integral Particular .2

sincos)(

:as written assolution w The

1for chapter). previousin (describedequation shomogeneou the

forsolution theisIt :response) (Transientfunction ary Complement 1.

parts two

hassolution Its .homogenuos-non isequation aldifferentiorder 2nd This

(1)motion ofEquation ...

:form heConsider t

21

tjp

ddt

c

tjo

ex

tCtCetx

eFkxxcxm

n

Harmonically Excited Vibration

amplitude. response statesteady

theof magnitude"" thedenotes X , X

as written be nowcan integral particular for the There

X re wheXX

Response. and Forcebetween angle"

phase" theis tan where,

as By writing

X

:Xfor solve and (1)equation into integral particular theSubstitute

222

21-222

2

2

tjp

oj

j

o

ex

cmk

Fe

mk

cwecmk

jcmk

jcmk

F

Harmonically Excited Vibration

motion. theof conditions inatial theknowing

from dermined be toconstants are C2 and C1 that Note

X sincos)(

)()()(

:is (1)motion ofequation for the (response)solution totalThe

1

2tan

ratio.frequency theis where, 21

X

:as written bemay and X

21

21

222

tjdd

t

pc

n

o

etCtCetx

txtxtx

r

r

rrr

k

F

n

Harmonically Excited Vibration

222

st

sto

21

1M

(M)".Factor ion Magnificat" thecalledusually is

ratio The ).( deflection static" thecalledusually is k

F termThe .5

.frequency and amplitude

constant h motion wit harmonic a is ))(( response stateSteady 4.

me.certain ti aafter neglected becan and time

with decayst motion tha a represents ))(( responseTransient .3

cos)(cos form force For the 2.

sin)(sin form force For the 1.

:NOTES

rr

X

tx

tx

tXtxtFF(t)

tXtxtFF(t)

p

c

po

po

Damped Forced Vibration System

Graphical representation for Magnification factor M and ϕ.

Damped Forced Vibration System

Notes on the graphical representation of X.

For ζ = 0 , the system is reduced and becomes un-

damped.

for any amount of ζ > 0 , the amplitude of

vibration decreases (i.e. reduction in the

magnification factor M). This is correct for any

value of r.

For the case of r = 0, the magnification factor

equals 1.

The amplitude of the forced vibration

approaches zero when the frequency ratio ‘r’

approaches the infinity (i.e. M→0 when r → ∞)

Damped Forced Vibration System

Notes on the graphical representation for ϕ.

For ζ = 0 , the phase angle is zero for 0<r<1 and

180o for r>1.

For any amount of ζ > 0 and 0<r<1 , 0o<ϕ<90o.

For ζ > 0 and r>1 , 90o<ϕ<180o.

For ζ > 0 and r=1 , ϕ= 90o.

For ζ > 0 and r>>1 , ϕ approaches 180o.

Harmonically Excited Vibration

) small(for is

ntdisplaceme themeans which 2

X then 1)(r resonanceAt 3.

is

ntdisplaceme themeans which X then 1)(rfrequency high At 2.

is

ntdisplaceme themeans which X then 0)(rfrequency lowAt 1.

amplitude response s.s theis 21

X

: have We

:frequencynt with displaceme ofVariation

2

222

control.Damping

control. Mass

control. Stiffness

k

F

m

F

k

F

rr

kF

o

o

o

o

Harmonically Excited Vibration

2res

2

1/2-222

21 i.e

a asknown is which 21 when maximum is X

:givescondition This

0)X( when maximum is X

21 X

:as written becan amplitude response s.s The

n

n

o

r

dr

d

rrk

F

Frequency,Resonance

:amplitude Maximum ofFrequency

Forced Vibration due to Rotating Unbalance

tmekxxcxM t sin...

2

Forced Vibration due to Rotating Unbalance

below figure in theshown are and X of plots The

1

2tan

and

21X

or ,21

X

21

222

2

222

2

r

r

rr

rMme

rr

kme

t

Transmissibility of Force

)r-(1

r2tan ,

)2()1(

)2(1TR

TR bility,Transmissi Force theas TR define

)(

)(F

i.e, motion harmonic Assume

F

is foundation the toed transmittforce then the

,neglugible is foundation of deflection theIf

21

22

2

F

2tr

tr

rr

r

F

F

cjmk

Fcjk

Xex

xckxe

F

o

tr

F

o

tj

tj

Transmissibility of displacement (support motion)

Physical system:

Mathematical model: 0....

yxkyxcxm

The forcing function for the base excitation

Transmissibility of displacement (support motion)

Substitute the forcing function into the math. Model:

motion) (Harmonict Xsin x(t)Assume

tan

:Where

sincossin...

1

22

k

c

ckYA

tAtYctkYkxxcxm

2

1

222

2

222

22

d

1

2tan

21

21)bility(TRTransmissint Displaceme

r

r

rr

r

cmk

ck

Y

X

Transmissibility of displacement (support motion)

Graphical representation of Force or Displacement Transmissibility ((TR) and the Phase angle (

Example 3.1: Plate Supporting a Pump: A reciprocating pump, weighing 68 kg, is mounted at

the middle of a steel plate of thickness 1 cm, width 50 cm, and length 250 cm. clamped along two edges as shown in Fig. During operation of the pump, the plate is subjected to a harmonic force, F(t) = 220 cos (62.832t) N. if E=200 Gpa, Find the amplitude of vibration of the plate.

Example 3.1: solution

The plate can be modeled as fixed – fixed beam has the following stiffness:

The maximum amplitude (X) is found as:

mNx

xxkSo

mxxxbhIBut

l

EIk

/ 82.400,10210250

10667.4110200192 ,

10667.41101105012

1

12

1

192

32

99

493223

3

mmmk

FX o 32487.1

832.626882.400,102

2202

-ve means that the

response is out of phase

with excitation

Example 3.2:Find the total response of a single-degree-of-

freedom system with m = 10 kg, c = 20 N-s/m, k=4000 N/m, xo = 0.01m and = 0 when an external force F(t) = Fo cos(ωt) acts on the system with Fo = 100 N and ω = 10 rad/sec .

Solution a. From the given data

ox.

sradm

kn /20

10

4000

05.020102

20

2

nm

c

sradd

d

nd

/975.19

2005.01

1

2

2

5.020

10

n

r

Example 3.2: Solution

Total solution:X(t) = X c (t) + X p(t)

mk

Fost 025.0

4000

100

mrr

X st 3326.021 222

o

r

r814.3

1

2tan

21

0.066)-0t20.3326cos()-cos(19.97t20*.050-

e (t)

0.066)-tcos(X)-tncos(-

e (t)

tAx

tnAx

0.066)-0t20.3326cos(- )066.0-cos(19.97t--6.64ex(t)

-0.3325A and rad 0.066

0.438,

0.066)-0t220sin(*0.3326

-(-t)e*)-(19.97tcos)-(19.97t-19.97sin *-e)(

0.066)-0t20.3326cos()-cos(19.97t-e (t)

(1) 33187.0cos

cos0.066*0.3326cos

(2) and (1) From

(2) 0219.0sinsin97.190

0 0,at t

0

01.0 0,at t

t

tAtAtx

tAx

A

A

AA

tx

mtx