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Theory of Elasticity Chapter 11 Bending of Thin Plates 薄薄薄薄

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Theory of Elasticity. Chapter 11 Bending of Thin Plates 薄板弯曲. Theory of Elasticity. Page. Chapter. Content. Introduction Mathematical Preliminaries Stress and Equilibrium Displacements and Strains Material Behavior- Linear Elastic Solids Formulation and Solution Strategies - PowerPoint PPT Presentation

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Page 1: Theory of Elasticity

Theory of Elasticity

Chapter 11Bending of Thin Plates

薄板弯曲

Page 2: Theory of Elasticity

Chapter Page

Content• Introduction• Mathematical Preliminaries • Stress and Equilibrium• Displacements and Strains• Material Behavior- Linear Elastic Solids• Formulation and Solution Strategies• Two-Dimensional Problems• Three-Dimensional Problems• Bending of Thin Plates (薄板弯曲)• Plastic deformation - Introduction• Introduction to Finite Element Method

11 1

Page 3: Theory of Elasticity

Bending of Thin Plates

• 11.1 Some Concepts and Assumptions(有关概念及假定)• 11.2 Differential Equation of Deflection(弹性曲面的微分方程)• 11.3 Internal Forces of Thin Plate(薄板截面上的内力)• 11.4 Boundary Conditions (边界条件)• 11.5 Examples (例题)

Chapter Page 11 2

Page 4: Theory of Elasticity

11.1 Some Concepts and Assumptions

Chapter Page

Thin plate (薄板)

11 3

One dimension of which (the thickness)is small in comparison with the other two. ( 1/8 - 1/5 ) >/b≥ ( 1/80-1/100 )

Middle surface( 中面 )

The plane of Z=0

Bending of thin plate (薄板弯曲)

Only transverse loads act on the plate. (垂直于板面的载荷,横向)

Longitudinal loads: Plane stress State

Similar with Bending of elastic beams

Page 5: Theory of Elasticity

11.1 Some Concepts and Assumptions

Chapter Page

Review: bending of beams

11 4

Page 6: Theory of Elasticity

11.1 Some Concepts and Assumptions

Chapter Page

Assumptions(beam):

1, The plane sections normal to the longitudinal axis of the beam remained plane ( 平面假设 )2, In the course “elementary strength of materials”: simple stress state :only normal stress exists, no shearing stress. Pure bending(单向受力假设)

11 5

Page 7: Theory of Elasticity

11.1 Some Concepts and Assumptions

Chapter Page

Assumptions for bending of thin plate ( Kirchhoff)

Besides of the basic assumptions of “Theory of elasticity”

1,Straight lines normal to the middle surface will remain straight and the same length. 变形前垂直于中面的直线变形后仍然保持直线,而且长度不变。

2,Normal stresses transverse to the middle surface of the plate are small and the corresponding strain can be neglected. 垂直于中面方向的应力分量 z, τzx , τzy远小于其他应力分量,其引起的变形可以不计 .

3,The middle surface of the plate is initially plane and is not strained in bending. 中面各点只有垂直中面的位移 w,没有平行中面的位移

11 6

Page 8: Theory of Elasticity

11.1 Some Concepts and Assumptions

Chapter Page

1,Straight lines normal to the middle surface will remain straight and the same length. 变形前垂直于中面的直线变形后仍然保持直线,而且长度不变。

Physical Equation Reduced to 3

or

or

11 7

Page 9: Theory of Elasticity

11.1 Some Concepts and Assumptions

Chapter Page

2,Normal stresses transverse to the middle surface of the plate are small and the corresponding strain can be neglected. 垂直于中面方向的应力分量 z, τzx , τzy 远小于其他应力分量,其引起的变形可以不计 .

11 8

Page 10: Theory of Elasticity

11.1 Some Concepts and Assumptions

Chapter Page

3,The middle surface of the plate is initially plane and is not strained in bending. 中面各点只有垂直中面的位移 w,没有平行中面的位移

uz=0=0 , vz=0=0 , w=w(x, y)

11 9

Page 11: Theory of Elasticity

11.2 Differential Equation of Deflection弹性曲面的微分方程

Chapter Page

Displacement Formulation

The equilibrium equation is expressed in terms of displacement. w

Besides w, the unknowns include

Displacement:

u, v

Primary strain Components: xyyx ,,

0,, zxzyz

Primary stess Components: xyyx ,,

。xyxy

xyy

yxx

E

12

,E

1

,E

1

Secondary stess Components: zzyzx ,

)(,,, wfvu

11 10

Page 12: Theory of Elasticity

11.2 Differential Equation of Deflection

Chapter Page

u, v in terms of w

0,0 zyzx 。y

w

z

v,

x

w

z

u

zy

wv,z

x

wu

uz=0=0 , vz=0=0

xyyx ,,

εx , εy , γxy in terms of w

。zyx

w2

y

u

x

v

,y

w

y

u,

x

w

x

u

2

xy

2

2

y2

2

x

u-ε Relations

11 11

Page 13: Theory of Elasticity

11.2 Differential Equation of Deflection

Chapter Page

x , y , τ xy in terms of w

Physical Equations

。zyx

w2

y

u

x

v

,y

w

y

u,

x

w

x

u

2

xy

2

2

y2

2

x

。yx

w

1

Ez

,x

w

y

w

1

Ez

,y

w

x

w

1

Ez

2

xy

2

2

2

2

2y

2

2

2

2

2x

11 12

Page 14: Theory of Elasticity

11.2 Differential Equation of Deflection

Chapter Page

τ xz , τ yz in terms of w

。wy4

z12

E

,wx4

z12

E

22

22zx

22

22zx

The equilibrium equation

11 13

Page 15: Theory of Elasticity

11.2 Differential Equation of Deflection

Chapter Page

z in terms of w

。y,xFw3

zz

412

E 432

2z

。wz

1z

2

1

16

E

w8

z3

1

2z

412

E

42

2

43

32

2z

If body force fz≠0:

)(,,,,,,,,,, zyzxxy wfvu xyyxzyx

11 14

Page 16: Theory of Elasticity

11.2 Differential Equation of Deflection

Chapter Page

The governing equation of the classical theory of bending of thin elastic plates:

q2

zz

qwD 4 ,2

3

112

ED

。wz

1z

2

1

16

E

w8

z3

1

2z

412

E

42

2

43

32

2z

qw112

E 42

3

Flexural rigidity of the plate

11 15

Page 17: Theory of Elasticity

11.2 Differential Equation of Deflection

Chapter Page

)(, wfvu )(,, wfxyyx

)(,, wfxyyx

)(, zyzx wf

Geometrical Equations

Physical Equations

Equilibrium Equations

Boundary Cond. (load:q))(z wf

qwD 4 +edges B.C.

11 16薄板的弹性曲面微分方程

Page 18: Theory of Elasticity

11.2 Differential Equation of Deflection

Chapter Page

Another method to get the equation

11 17

Page 19: Theory of Elasticity

11.2 Differential Equation of Deflection

Chapter Page

History of the Equation

Bernoulli, 1798:

Beam Thin plate

Lagrange, 1811:

11 18

Page 20: Theory of Elasticity

11.3 Internal Forces of Thin Plate

Chapter Page

Internal Forces:

Stress resultants: It is customary to integrate the stresses ovet the constant plate thickness defining stress reslultants. 薄板截面的每单位宽度上,由应力向中面简化而合成的主矢量和主矩。

Design requirement( 薄板是按内力来设计的; )Dealing with the Boundary Conditions( 在应用圣维南原理处理边界条件,利用内力的边界代替应力边界条件。 )

11 19

Page 21: Theory of Elasticity

11.3 Internal Forces of Thin Plate

Chapter Page

x

xM

y

x

zxy

xyM

xz

Fsx

。yx

w

1

Ez

,x

w

y

w

1

Ez

,y

w

x

w

1

Ez

2

xy

2

2

2

2

2y

2

2

2

2

2x

。wy4

z12

E

,wx4

z12

E

22

22zy

22

22zx

11 20

Page 22: Theory of Elasticity

11.3 Internal Forces of Thin Plate

Chapter Page

Stress distribution

。yx

w

1

Ez

,x

w

y

w

1

Ez

,y

w

x

w

1

Ez

2

xy

2

2

2

2

2y

2

2

2

2

2x

。wy4

z12

E

,wx4

z12

E

22

22zy

22

22zx

。 2

2

xx dzzM

。 2

2

xyxy dzzM

。 2

2

xzSx dzF

11 21

Page 23: Theory of Elasticity

11.3 Internal Forces of Thin Plate

Chapter Page

。 2

2

xx dzzM

。 2

2

xyxy dzzM

。 2

2

xzSx dzF

2

2

2

2

2

3

2

2

22

2

2

2

2x

y

w

x

w

112

E

dzzy

w

x

w

-1

EM

。yx

w

112

E

dzzyx

w

1

EM

23

2

2

22

xy

wx-112

E

dz4

zwx-12

EF

22

3

2

2

222

2Sx

11 22

Page 24: Theory of Elasticity

11.3 Internal Forces of Thin Plate

,2

3

112

ED

Chapter Page

。wy

-DF,wx

-DF

,yx

w1DMM

,x

w

y

wDM,

y

w

x

wDM

2Sy

2Sx

2

yxxy

2

2

2

2

y2

2

2

2

x

11 23

Page 25: Theory of Elasticity

11.3 Internal Forces of Thin Plate

Chapter Page

应力分量 和内力、载荷关系 名称 数值

最大

最大

较小

最小

11 24

Page 26: Theory of Elasticity

11.4 Boundary Conditions

Chapter Page

qwD 4 +edges B.C.

Simply Supported edge 简支边界

Free edge 自由边界

Built-in or clamped edge 固定边界

11 25

Page 27: Theory of Elasticity

11.4 Boundary Conditions

Chapter Page

Built-in or clamped edge 固定边界

。0x

w,0w

0x0x

At a clamped edge parallel to the y axis:

11 26

Page 28: Theory of Elasticity

11.4 Boundary Conditions

Chapter Page

Simply Supported edge 简支边界

Free to rotate

The bending moment and the deflection along the edge must be zero.

。0M,0w0yy0y

。0x

w

y

w,0w

0y2

2

2

2

0y

。0y

w,0w

0y2

2

0y

11 27

Page 29: Theory of Elasticity

11.4 Boundary Conditions

Free edge 自由边界

Chapter Page

。0F,0M,0MbySybyyxbyy

x

MFF yxsysy

t

0,0

x

MFFM yxsysy

ty

0yx

w2

y

w

,0x

w

y

w

by

2

3

3

3

by

2

2

2

2

Only 2 are allowed for an equation of 4th order

11 28

Page 30: Theory of Elasticity

11.5 Examples: Simple supported rectangular plate

Chapter Page

An application of plate theory to a specific problem

Problem: Calculating the deflection w of a simply supported rectangular plate as shown in the fig., which is loaded in the z direction by a load of q(x,y) Solution:

Boundary conditions:

11 29

Page 31: Theory of Elasticity

11.5 Examples:Simple supported rectangular plate

Chapter Page

The plate deflection must satisfy the following equation and the boundary conditions.

qwD 4 Choose to represent w by the double Fourier series:

All the boundary conditions are satisfied. Substituted into we obtain:

11 30

Page 32: Theory of Elasticity

11.5 Examples: Simple supported rectangular plate

Chapter Page

If q(x,y) were represented by Fourier series, It might be possible to match coefficients. Expand q(x,y) in a Fourier series.

W

11 31

Page 33: Theory of Elasticity

Homework

• 9-1

Chapter Page 11 32