04 vibration of bars
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Dynamics of Continuous StructuresMaged Mostafa
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Vibration of Continuous Structures
Dynamics of Continuous StructuresMaged Mostafa
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Bar Vibration
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Course Contents SDOF M-DOF Cables/String• Bars• Shafts• Vibration Attenuation• Beams• FEM for Vibration• Plates• Aeroelasticity
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Objectives
• Derive the equation of motion for Bars• Estimate the Natural Frequencies• Understand the concept of mode shapes• Apply BC’s and IC’s to obtain structure
response
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Objectives
• Derive the equation of motion for Bars• Apply BC’s and IC’s to obtain structure
response• Estimate the Natural Frequencies• Understand the concept of mode shapes
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Bar Vibration
• The bar is a structural element that bears compression and tension loads
• It deflects in the axial direction only• Examples of bars may be the columns of
buildings, car shock absorbers, legs of chairs and tables, and human legs!
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Vibration of Rods and Bars
• Consider a small element of the bar
• Deflection is now along x (called longitudinal vibration)
• F= ma on small element yields the following:
x x +dx
u(x,t) x
dx
F+dF F
Equilibrium position
Infinitesimal element
0 l
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Remember!
xtxuxEAF
xtxu
ExσAF
From
),()(
),(
)(Law sHawk'
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0
),( :end free At the
,0),0( :end clamped At the
),(
),( constant)(
),( )(
),()(
),()(
),()(
),( )(
2
2
2
2
2
2
2
2
xxtxuEA
twt
txux
txuExA
ttxuxA
xtxuxEA
x
dxx
txuxEAx
dFx
txuxEAF
ttxudxxAFdFF
Force balance:
Constitutive relation:
Dynamics of Continuous StructuresMaged Mostafa
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Objectives
• Derive the equation of motion for Bars• Apply BC’s and IC’s to obtain structure
response• Estimate the Natural Frequencies• Understand the concept of mode shapes
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Apply the boundary conditions to the spatial solution to get
asin(0) bcos(0)0acos( l ) bsin( l )0
b 0 and det0 1
cos( l ) sin( l )
0
cos l 0 n
2n 12l , n 1,2,3,L
Xn (x)an sin((2n 1) x
2l ), n 1,2, 3,L
Dynamics of Continuous StructuresMaged Mostafa
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Objectives
• Derive the equation of motion for Bars• Apply BC’s and IC’s to obtain structure
response• Estimate the Natural Frequencies• Understand the concept of mode shapes
Dynamics of Continuous StructuresMaged Mostafa
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time response equation :
Tn (t) c2 2n 12l
2
T (t)0
Tn (t)An sin(2n 1)c
2l t Bn cos(2n 1)c
2l t
n (2n 1)c
2l (2n 1)
2lE
, n 1,2,3L (6.63)
Thus the solution implies oscillation with Frequencies:
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Note
• The equation of motion of the bar is similar to that of the cable/string the response should have similar form
• The bar may have different boundary conditions
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Given v0(l)=3 cm/s, =8x103 kg/m3 and E=20x1010 N/m2, compute the response.
w(x,t) (cn sin nctn1
dn cos nct)sin(2n 1)
2l x
dn 2l w0 (x)sin
0
l
(2n 1)
2l xdx 0
wt (x,0)0.03 (x l ) cn nccos(0)n1
sin(2n 1)
2l x
0
Multiply by the mode shape indexed m and integrate:
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0.03 (sin0
l
(2m 1)
2l x) (x l )dx
cn0
l
ncsinn1
(2m 1)2l x sin
(2n 1)2l xdx
0.03sin(2m 1)
2
cml2
cm cm 1
E
0.06( 1)m1
(2m 1)
cn 8103
210109
0.12( 1)n1
(2n 1)7.45510-6 ( 1)n1
(2n 1) m
w(x, t)7.45510-6 ( 1)n1
(2n 1)sin
2n 110
x
n1
sin 512.348(2n 1)t m
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Assignment
• Solve the equation of motion of a bar with constant cross-section properties with
1. Fixed-Fixed boundary conditions2. Free-Free boundary conditions
• Compare the natural frequencies for all three cases
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