Uni Seminar

Preview:

Citation preview

Advanced FEACoded in Matlab

JL Mantari, PhD

Contents• Plates theories

• Accuracy problem

• New theories

• FEA simple applications

• FEA layerwise

• FEA applications

Plate theories Existing theories

CPT (Classical plate theory), based on the assumptions of Kirchhoff’s plate theory.

FSDT (First order shear deformation theory), assumes constant transverse shear deformation and violates free surface boundary conditions.

).,(),,(

,),(),,(

,),(),,(

yxwzyxw

y

wzyxvzyxv

x

wzyxuzyxu

).,(),,(

,),(),,(

,),(),,(

yxwzyxw

zyxvzyxv

zyxuzyxu

y

x

HSDT (Higher order shear deformation theory), assumes adequate transverse shear deformation and comply free surface boundary conditions.

f(z)).,(),,(

,),(),,(

,),(),,(

3*

3*

yxwzyxw

zy

wyzyxvzyxv

zx

wyzyxuzyxu

yy

xx

Plate theories Existing theories

ESL (Equivalent single layer) theories: CPT (Classical plate theory),FSDT (First shear deformation theory),HSDT (Higher order shear deformation theory),Others

Plate theories Existing theories

Layerwise theories:FSDTHSDTOthers

Plate theories Existing theories

Plate theories Accuracy problem

For unstiffened and stiffened ship type structures, HSDTs should be used because the deformation field is close to the deformation in real situation.

Variation of central deflection (mm) with varying geometric configurations

HSDTs

Plate theories Well-know HSDTs

,

,

.

).,(),,(

,)sinh(),(),,(

,)sinh(),(),,(

22*

11*

yxwzyxw

h

z

y

wyzyxvzyxv

h

z

x

wyzyxuzyxu

HSDT1

HSDT2

).,(),,(

,)sin(),(),,(

,)sin(),(),,(

22*

11*

yxwzyxw

h

z

y

wyzyxvzyxv

h

z

x

wyzyxuzyxu

).,(),,(

,),(),,(

,),(),,(

23

2*

13

1*

yxwzyxw

zy

wyzyxvzyxv

zx

wyzyxuzyxu

HSDT3

Plate theories New GHSDTs

,

,

.

GHSDT1

GHSDT2

FEA Simple applications

Plates special case of shells. Beams special case of plates. Then, curved beams are special case of shells!

Beams Plates

Shells FGP

FEA bases A unified theory

,

,

.

Assume the following displacement field to begin the derivation of the unified theory I.

Laminate analysis. Steps for the validation of the theory

,

,

.

Displacement field.Elasticity theory to get strains.Law of Hook to get stresses.The principle of virtual work and the variational theory to get,A set of differential equations that govern the plate and finally,Solve it with an appropriated solution (closed-form).

D E L T A S

Laminate analysis. Finite element method

,

,

.

Displacement field.Elasticity theory to get strains.Law of Hook to get stresses.The principle of virtual work, then use the discretization.Apply boundary conditions, and finallySolve it!

D E L T A S

1. When ESL FE codes are implemented by using: FSDT

A (Cº) FEM code can be implemented Requires arbitrary shear correction factors No comply free surface boundary condition

HSDT A (C ) FEM need to be implemented Normally non-conforming FEM are implementedA (Cº) FEM code can be also achieved

2. FEM using FSDT and HSDT have been explored since 1960s.

3. Layerwise FE codes do not need shear correction factors as some well-know ESL HSDT.

4. A new generalized layerwise HSDT is presented in this thesis.

Laminate analysis. Existing theories (FEM)

Laminate analysis. Trigonometric layerwise HSDT(FEM)

),( yxww oin

Inner layer

ex

in

xcin

xin

xin

inc

ink

xkk

xc

cinin mamz

x

wz

hh

h

x

wau ')tan()(

22

ycin

yin

yin

inc

ink

ykk

yc

cinin mamz

y

wz

hh

h

y

wav ')tan()(

22

z

u x

w

x

x

x3

4x

Layer 5

Layer 4

Layer 3

Layer 2

Layer 1

x

h

h

h

h

h5

4

3

2

1

w

z

x

x

u

x

x

xu

x

x

o o

-z wx

f(z) 3'

5x

x1

x2

Laminate analysis. Generalized layerwise HSDT

),( yxww oin

Inner layer

ex

in

xcin

xin

xin

inc

ink

xkk

xc

cinin azf

x

wz

hh

h

x

wau ')()(

22

ycin

yin

yin

inc

ink

ykk

yc

cinin azf

y

wz

hh

h

y

wav ')()(

22

z

u x

w

x

x

x3

4x

Layer 5

Layer 4

Layer 3

Layer 2

Layer 1

x

h

h

h

h

h5

4

3

2

1

w

z

x

x

u

x

x

xu

x

x

o o

-z wx

f(z) 3'

5x

x1

x2

Laminate analysis. Reducing DOFs

Shear continuity imposed

xchinin

in

inininxin in

azfQ

QD

Q

QD

Q

QD '

255

1

551

55

2

552

55

1

551 ))('...(

ychinin

in

inininyin in

azfQ

QD

Q

QD

Q

QD '

244

1

441

44

2

442

44

1

441 ))('...(

xchexex

ex

exexexxex ex

azfQ

QD

Q

QD

Q

QD '

255

1

551

55

2

552

55

1

551 ))('...(

ychexex

ex

exexexyex ex

azfQ

QD

Q

QD

Q

QD '

244

1

441

44

2

442

44

1

441 ))('...(

iD22

)(')('ii hihi azfazf excini ,,

where

Laminate analysis. Energy principle (FEM)

,

,

.

,

.

Four-nodded quadrilateral Cº continuous isoparametric element with five-degrees-of-freedom (shear continuity is imposed)

n

iiiN

1

B

extse WU

l

k

T

V

l

k

kTTs

dxdyD

dxdydzQdVU

1

1

}]{[}{2

1

}]{[}{2

1

2

1

dxdyqwW oext

dzHQHDkl

k

T ]][[][][1

Laminate analysis. Integration scheme (FEM)

,

,

.

,

.

qdNdBDB TwTTTe

o ][}{}]{][[][}{2

1

}{}{}}{{}{2

1e

Te

T PK

dBDBK Te ]][[][][

qdNP Twe

o ][][

}{}]{[ ee PK

Laminate analysis. Applications

Beams Plates

Stiffened plates FGP

Recommended