Membranes and thin plates

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Vibration of Continuous Structures

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Vibration of Membranes &Thin Plates

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Course ContentsSDOF M-DOFCables/String Bars Shafts Vibration Attenuation Beams Membranes & Thin Plateso FEM for Vibrationo Aeroelasticity

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Vibration of Membranes

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Objectives

• What is Membrane?• The equation of motion for membranes

• 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

• What is Membrane?• The equation of motion for membranes

• Estimate the Natural Frequencies• Understand the concept of mode shapes• Apply BC’s and IC’s to obtain structure response

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What is Membrane?• 2-D material (Structure) does not resist

bending• Analogous to cables• Examples:

• Tents• Human Tissues• Light Aircraft

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Objectives

• What is Membrane?• Derive the equation of motion for

membranes• Estimate the Natural Frequencies• Understand the concept of mode shapes• Apply BC’s and IC’s to obtain structure response

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Equations of Motion• The structure itself does not resist

bending, so the restoring force is due only to the tension

w: Out of plane displacement: tension per unit length : mass per unit area Laplace operator in Cartesian coordinates:

),,(w ),,(w2 tyxtyx tt

2

2

2

22

yx

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Equations of Motion

Boundary Conditions are defined along the shape of the boundaries not just a point!!

c

tw

cyw

xw

2

2

22

2

2

2 1

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Rectangular Membrane• Using Separation of variables:

22222

2

22

22

, ,

1

1

YY

XX

YY

XXTT

c

TT

cYY

XX

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Rectangular Membrane• Solve the 3 ODEs:

)cos()sin()(0

)cos()sin()(0

)cos()sin()(0

22

2

2

tcHtcFtTTcT

yDyCyYYY

xBxAxXXX

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Rectangular Membrane• Total Spatial Solution

)cos()cos()sin()cos()cos()sin()sin()sin(),(

)()(),(

43

21

yxAyxAyxAyxAyxW

yYxXyxW

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Apply Boundary Conditions• Clamped Along all boundaries

)cos()sin()sin()sin(),(

0)cos()sin(

)()0(0),0(

21

43

43

yxAyxAyxW

AAyAyA

yYXyW

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Apply Boundary Conditions• Clamped Along all boundaries

bm

an

yAyAayYaX

yaW

:Similarly

solution trivial-nonfor

)cos()sin()sin()()(

0),(

21

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Natural Frequencies• Clamped Along all boundaries

ybmSinx

anSin

nmbm

an

mnmn

:ionsEigenfucnt

,...,3,2,1, ,22

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Full Solution• Clamped Along all boundaries

ctBctA

ybmx

antyxw

mnmn

mnmn

m n

cossin

sinsin,,

:Solution Full

1 1

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Using orthogonality to evaluate the remaining constants from the initial conditions

Recall

nmmnmn

dxxmxn 2 ,0

,)sin()sin( 2

0

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Using orthogonality to evaluate the remaining constants from the initial conditions

ctBctAab

dxdyybmx

antyxw

mnmnmnmn

b a

cossin4

sinsin,,0 0

This leads to

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Using orthogonality to evaluate the remaining constants from the initial conditions

dxdyybmx

anyxw

cabB

dxdyybmx

anyxw

abA

b a

mnmn

b a

mn

0 0

0 0

sinsin0,,4

sinsin0,,4

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Homework• Draw the first 3 mode shapes for

square membrane with side length =1 and all sides are clamped

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Vibration of Plates

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Objectives

• What is Plate?• The equation of motion for Plates

• 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

• What is Plate?• The equation of motion for Plates

• Estimate the Natural Frequencies• Understand the concept of mode shapes• Apply BC’s and IC’s to obtain structure response

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What is Plate?• 2-D material (Structure) that can resist

bending• Analogous to beam• Examples

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Objectives

• What is Plate?• The equation of motion for Plates

• Estimate the Natural Frequencies• Understand the concept of mode shapes• Apply BC’s and IC’s to obtain structure response

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Equations of Motion• Assume small deflections with respect to the

thickness h.• Normal stresses transverse to the plate is

negligible

Where:

),,(w ),,(w4 tyxtyxD ttE

4

4

22

4

4

44 2

yyxx

2

3

112

EhDE

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Boundary Conditions

Clamped:

Simply Supported:

0 ),,(w ,0 ),,(w

ntyxtyx

0 ),,(w

,0 ),,(w

2

2

ntyx

tyx

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