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Chapter 5 Two Degrees of Freedom

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Page 1: Chapter 5 Two Degrees of Freedom
Page 2: Chapter 5 Two Degrees of Freedom

Systems that require two independent coordinates to describe their motion are called Two Degree of Freedom Systems.

Page 3: Chapter 5 Two Degrees of Freedom

Systems that require two independent coordinates to describe their motion are called Two Degree of Freedom Systems.

Page 4: Chapter 5 Two Degrees of Freedom

The general rule for the computation of the number of freedom

Number of Degrees of

freedomof the system

Number of masses in the systemx=

number of possible types of motion of each mass

Page 5: Chapter 5 Two Degrees of Freedom

There are two equations of motion for a two degree of freedom system, one for each mass/DOF.

They are in the form of coupled differential equation- that is, each equation involves all coordinates

If harmonic solution is assumed for each coordinate, the equation lead to a frequency equation that gives two natural frequencies

Page 6: Chapter 5 Two Degrees of Freedom

Given a suitable initial excitation, the system vibrates at one of these natural frequencies

During free vibration at one of the natural frequencies, the amplitude of the TDOF are related in a specific manner and the configuration is called a normal mode, principal mode, or natural mode

If the system vibrates under the action of an external harmonic force , the resulting forced harmonic vibration takes place at the frequency of the applied force

Page 7: Chapter 5 Two Degrees of Freedom

Resonance occurs when the forcing frequency is equal to one of the natural frequencies of the system

The configuration of a system can be specified by a set of independent coordinates such as length, angle, or other physical parameter. Generalized coordinates

A set of coordinates which leads to an uncoupled equations of motions are called principal coordinates

Page 8: Chapter 5 Two Degrees of Freedom

1221212212111 Fxkxkkxcxccxm

2232122321222 Fxkkxkxccxcxm

Page 9: Chapter 5 Two Degrees of Freedom

tFtxktxctxm

2

1

0

0

m

mm

322

221

ccc

cccc

Page 10: Chapter 5 Two Degrees of Freedom

tFtxktxctxm

322

221

kkk

kkkk

tx

txtx

2

1

tF

tFtF

2

1

Page 11: Chapter 5 Two Degrees of Freedom

tFtxktxctxm

The solution involves four constant of integration. From the initial conditions;

00,00

00,00

2222

1111

xtxxtx

xtxxtx

Page 12: Chapter 5 Two Degrees of Freedom

00 32121 ccctFtF

02212111 txktxkktxm

02321222 txkktxktxm

tXtx cos11

tXtx cos22

Page 13: Chapter 5 Two Degrees of Freedom

0cos22121

2

1 tXkXkkm

0cos232

2

212 tXkkmXk

Equation 5.7

X1 and X2 are constants the maximum amplitude of x1 (t) and x2(t), φ is the phase angle.

Page 14: Chapter 5 Two Degrees of Freedom

022121

2

1 XkXkkm

0232

2

212 XkkmXk

0det

32

2

22

221

2

1

kkmk

kkkm

02

23221

2

131221

4

21

kkkkk

mkkmkkmm

nontrivial solution

Frequency or Characteristic equation

Page 15: Chapter 5 Two Degrees of Freedom

2/1

21

2

23221

2

21

132221

21

1322212

2

2

1

4

2

1,

mm

kkkkk

mm

mkkmkk

mm

mkkmkk

Natural frequencies of the system,

Page 16: Chapter 5 Two Degrees of Freedom

32

2

12

2

2

21

2

11

1

1

1

21

kkm

k

k

kkm

X

Xr

Frequencies ratios,

32

2

22

2

2

21

2

21

2

1

2

22

kkm

k

k

kkm

X

Xr

The normal modes of vibration (modal vectors),

1

11

1

1

1

2

1

11

Xr

X

X

XX

2

12

2

1

2

2

2

12

Xr

X

X

XX

Page 17: Chapter 5 Two Degrees of Freedom

The free vibration solution or the motion in time,

modefirst cos

cos

11

1

11

11

1

1

1

2

1

11

tXr

tX

tx

txtx

mode secondcos

cos

22

2

12

22

2

1

2

2

2

12

tXr

tX

tx

txtx

Page 18: Chapter 5 Two Degrees of Freedom

The unknown constant can be determine from the initial conditions,

2/1

2

1

2

2122

212

12

2/12

1

1

1

2

1

1

1

1

1

0000

1

sincos

xxrxxr

rr

XXtX

00,00

00,00

2222

1111

xtxxtx

xtxxtx

00

00tan

cos

sintan

2121

2121

1

1

1

1

1

11

1xxr

xxr

X

X

Page 19: Chapter 5 Two Degrees of Freedom

from the initial conditions,

2/1

2

2

2

2112

211

12

2/12

2

2

1

2

2

2

1

2

1

0000

1

sincos

xxrxxr

rr

XXX

00

00tan

cos

sintan

2112

2111

2

2

1

2

2

11

2xxr

xxr

X

X

Page 20: Chapter 5 Two Degrees of Freedom
Page 21: Chapter 5 Two Degrees of Freedom
Page 22: Chapter 5 Two Degrees of Freedom
Page 23: Chapter 5 Two Degrees of Freedom
Page 24: Chapter 5 Two Degrees of Freedom
Page 25: Chapter 5 Two Degrees of Freedom
Page 26: Chapter 5 Two Degrees of Freedom
Page 27: Chapter 5 Two Degrees of Freedom
Page 28: Chapter 5 Two Degrees of Freedom
Page 29: Chapter 5 Two Degrees of Freedom
Page 30: Chapter 5 Two Degrees of Freedom
Page 31: Chapter 5 Two Degrees of Freedom
Page 32: Chapter 5 Two Degrees of Freedom

Consider a torsional system consisting of two discs mounted on a shaft as shown below.

Parameters; k, J0 and Mt

11221111 ttt MkkJ

22312222 ttt MkkJ

Page 33: Chapter 5 Two Degrees of Freedom

12212111 tttt MkkkJ

22321222 tttt MkkkJ

Similar to the translational equations , but substituting θ → x, J → m, kt → k

0

0

Free Vibrations

Page 34: Chapter 5 Two Degrees of Freedom
Page 35: Chapter 5 Two Degrees of Freedom
Page 36: Chapter 5 Two Degrees of Freedom
Page 37: Chapter 5 Two Degrees of Freedom
Page 38: Chapter 5 Two Degrees of Freedom
Page 39: Chapter 5 Two Degrees of Freedom
Page 40: Chapter 5 Two Degrees of Freedom
Page 41: Chapter 5 Two Degrees of Freedom
Page 42: Chapter 5 Two Degrees of Freedom
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Page 45: Chapter 5 Two Degrees of Freedom

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