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Vibrations tutorial2, Exams of Food Science and Technology

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Elementary Tutorial
Prepared by Dr. An Tran
in collaboration with Professor P. R. Heyliger
Department of Civil Engineering
Colorado State University
Fort Collins, Colorado
June 2003
Fundamentals of Linear
Vibrations
Developed as part of the Research Experiences of Undergraduates Program on
“Studies of Vibration and Sound” , sponsored by National Science Foundation
and
Army Research Office (Award # EEC-0241979). This support is gratefully
acknowledged.
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Elementary Tutorial

Prepared by Dr. An Tran

in collaboration with Professor P. R. Heyliger

Department of Civil Engineering

Colorado State University

Fort Collins, Colorado

June 2003

Fundamentals of Linear

Vibrations

Developed as part of the Research Experiences of Undergraduates Program on

“Studies of Vibration and Sound” , sponsored by National Science Foundation

and

Army Research Office (Award # EEC-0241979). This support is gratefully

Fundamentals of Linear

Vibrations

1. Single Degree-of-Freedom

Systems

2. Two Degree-of-Freedom Systems

3. Multi-DOF Systems

4. Continuous Systems

A spring-mass system

General solution for any simple oscillator:

Governing equation of motion:

m  x   kx  0
( ) cos( ) sin( t )
v
x t x t n

n

o o n^  

  

2

n

(^2) o o

n n

n

o o o

ω

v ; C amplitude x 2

ω

T

1 f frequency(cycles/sec.or Hz)

; T periodof vibration T

2 naturalfrequency(rads/sec. ) m

k ω

x initialdisplacement; v initialvelocity x ; t time (sec.)

 

 

 

      

   

   

π

π

where:

Any simple oscillator

General approach:

1. Select coordinate system
2. Apply small displacement
3. Draw FBD
4. Apply Newton’s Laws:

( )

( )

I

dt

d M

m x

dt

d F

 

 

Simple oscillator – Example 2

l
a
m
k
I I md ml

n

cg

2 2

 

 

 

2 ( k a ) a ml

M I o o

 

 

0

2 2 ml   ka   

, ω (unstable) l

a As

m

k , ω l

a Notelimits: When

n

n

0 0

1

 

 

Simple oscillator – Example 3

 

  

 

^  

  

  

 

 

 (^)   

l

b

m

k ω

m ml m

ml

I I md

A l ml

I r dm x Adx

n

o cg

cg

l

3

12 2 3

12 12

2

2 2 2

2

(^32)

2 2 / 2

0

 

 

 

3

( )

2 ml k b b

M I o o

 

 

0

3

2

2

  kb  

ml 

Equivalent springs

Springs in series:

same force - flexibilities add

Springs in parallel:

same displacement - stiffnesses add

1 2

k k k eq

 

    

   

k k k eq

P k k

( 1 2 )

1 2

f f P f P

P k k

   eq

       

( )

1 1

1 2

1 2

1 2

1 2

f f f eq

 

Equivalent springs – Example 1

mxK x  0 eq 

0

12 3

3 2

3 1

 

   x

L

EI

L

EI mx

Equivalent springs – Example 3

0

2

2

 

 

 

 

 

ml mgl sin

Wl sin ml

M I o o

 

 

 

  sin   0

l

g 

l

g ω

l

g

n

We cannot define  n +

since we have sin  term

If  < < 1, sin    :

Energy methods

Strain energy U:

energy in spring = work done

Kinetic energy T:

Conservation of energy:

work done = energy stored

Uk   P  2

1

2

(^1 )

incrementofkineticenergy T

Incrementofwork done

    

 

(mr) (rdt) d( mr r) dT

F d r  

 

 

  

 

2

1

T mr r

Energy methods – Example

0

0

 

kxx mx x

(E ) dt

d

  

mx   kx  0

2 2

2

2

2

1

2

1

2

1

2

1

E U T kx m x

T m x

U kx

   

Same as vector mechanics

Work-energy principles have many

uses, but one of the most useful is

to derive the equations of motion.

Conservation of energy: E = const.

Two Degree-of-Freedom

Systems

1. Model problem

Matrix form of governing equation

Special case: Undamped free vibrations

Examples

2. Transformation of coordinates

Inertially & elastically coupled/uncoupled

General approach: Modal equations

Example

3. Response to harmonic forces

Model equation

Special case: Undamped system

Undamped free vibrations

Zero damping matrix [C] and force vector {P}

cos( ) 2

1

2

1    

  

t A

A

x

x

Assumed general solutions:

Characteristic polynomial (for det[ ]

=0):

0

1 2

(^212)

2

2

1

(^4 )   

 

  mm

k k

m

k

m

k k  

 

 

 

 

    

   

 

   

  

 

  

2

1

1 2

1 2

2

2

2

1

1 2

2

2

1

(^212)

2

1 2

1

4

2

1

m m

k k

m

k

m

k k

m

k

m

k k  

Eigenvalues (characteristic values):

Characteristic equation:

  

  

 

 

  

0

0

( )

( )

2

1 2 2 2 2

2

2 1 2 1

A

A

k k m

k k m k

Undamped free vibrations

Special case when k 1 =k 2 =k and m 1 =m 2 =m

Eigenvalues and frequencies:

fundamental period

fundamental frequency

 

 

ω

π T

m

k ω.

2

1 0618

m

k

  

 

  1. 618

  2. 3819 2 1

2 1

2

1 

 

Two mode shapes (relative participation of each mass in the motion):

1

2 1. 618 2

1

(^2)    k

k m

A

A  1 mode shape st 1

  1. 618 2 1

(^2)  

k m

k

A

A 2 mode shape

nd

The two eigenvectors are orthogonal:

  

  1. 618

1 ( 1 ) 2

( 1 ) 1 A

A

 

  1. 618

1 ( 2 ) 2

( 2 ) 1 A

A Eigenvector (1) = (^) Eigenvector (2) =