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58 Chapter III Finite element modelling and formulation development 3.1. General A structural analysis is performed on a model of the structure, not on the real structure, so the analysis can be no more accurate than the assumptions in the model. The model must represent the distribution and possible time variation of stiffness, strength, deformation capacity and mass of the structure with accuracy sufficient for the purpose of the analysis in the design process. In structural analysis, nonlinear modelling has evolved to address relevant issues including the variation in structural form, the influence of geometric nonlinearity and the nonlinear constitutive response of structural materials under serviceability and extreme loading conditions. In geotechnical analysis, on the other hand, developments have focused on, the constitutive modelling of different soils including pertinent nonlinear, coupling of mechanical/hydraulic/thermal/chemical processes in soils, and modelling of special boundary conditions, time dependent process such as consolidation and creep, and problem reduction. Though the structural field and geotechnical field have advanced computational tools offering sophisticated non-linear modelling in their respective fields, they fail together, to model an SSI problem to the same degree of sophistication. In this respect, existing advanced discipline-oriented computational tools are inadequate, on their own, for modelling a soil-structure interaction problem. One possibility is to augment existing software such that both soil and structure may be modelled to an equivalent level of sophistication though there remain significant technical challenges related to algorithmic and computational issues, particularly with reference to convergence. Another possibility is to develop new software integrating
Transcript

58

Chapter III

Finite element modelling and formulationdevelopment

3.1. General

A structural analysis is performed on a model of the structure, not on the real

structure, so the analysis can be no more accurate than the assumptions in the model.

The model must represent the distribution and possible time variation of stiffness,

strength, deformation capacity and mass of the structure with accuracy sufficient for the

purpose of the analysis in the design process.

In structural analysis, nonlinear modelling has evolved to address relevant issues

including the variation in structural form, the influence of geometric nonlinearity and the

nonlinear constitutive response of structural materials under serviceability and extreme

loading conditions.

In geotechnical analysis, on the other hand, developments have focused on, the

constitutive modelling of different soils including pertinent nonlinear, coupling of

mechanical/hydraulic/thermal/chemical processes in soils, and modelling of special

boundary conditions, time dependent process such as consolidation and creep, and

problem reduction.

Though the structural field and geotechnical field have advanced computational

tools offering sophisticated non-linear modelling in their respective fields, they fail

together, to model an SSI problem to the same degree of sophistication. In this respect,

existing advanced discipline-oriented computational tools are inadequate, on their own,

for modelling a soil-structure interaction problem.

One possibility is to augment existing software such that both soil and structure

may be modelled to an equivalent level of sophistication though there remain significant

technical challenges related to algorithmic and computational issues, particularly with

reference to convergence. Another possibility is to develop new software integrating

Non-linear Dynamic analysis of Soil Structure Interaction of Three Dimensional Structure For Varied Soil conditions

Chapter III

59

59

interdisciplinary computational model combining the features of both structural and

geotechnical aspects.

The powerful numerical tool like finite element method can be used to analyze the

problem considering the superstructure, foundation and the soil mass to act as single

integral compatible structural unit. As Finite element modelling and material modelling

depend on the method of dynamic analysis, summary of methods of analysis with their

advantages and disadvantages is presented below.

Further, of the four methods of SSI analyses viz., i) Elimination method, ii) Sub-structure

method, iii) Direct method and iv) Coupled methods of analysis, Direct Method of

analysis by using Finite element method is the only method that can be applied for non-

linear dynamic analysis of soil-structure-problem in time domain with the limitations of

other methods.

A suitable model can be picked up depending on the accuracy required and computational

facility available. Though it time consuming and necessitates development of a new soft

ware the present work deals with inclusion of non-linearity of soil in static and dynamic

SSI analysis of Space frame - foundation -soil system including the effects of infilled

masonry thoroughly investigating the effects of bonding between foundation and soil.

The solution of the problem of such interaction system needs a proper physical modelling

and numerical analysis to assess the more realistic and accurate structural behaviour of

the composite system.

3.2. Idealization of soil-structure interaction problem.

3.2.1. Modelling of superstructure

The various elements at macroscopic level in a three dimensional SSI problem are shown

in figure 3.1. The discretization of the domain of interaction system by adopting FEM

needs variety of isoparametric elements with different degrees of freedom.

All structures are three dimensional, but it is important to decide whether to use a

three-dimensional model or simpler two-dimensional models. The analysis methods are

the same whether the model is two dimensional or three dimensional. Generally, two

Non-linear Dynamic analysis of Soil Structure Interaction of Three Dimensional Structure For Varied Soil conditions

Chapter III

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60

dimensional models are acceptable for buildings with regular configuration and minimal

torsion; otherwise, a three-dimensional model is necessary with a representation of the

floor diaphragms, foundation and soil. M. Leipold (2009) categorized various frame

elements in to four types as mentioned in figure 3.2.

In the most generalized form, superstructure of the building frames may be idealized as

three-dimensional space frame using two nodded beam elements. Plate element of

suitable dimension may be added to mimic the behaviour of slabs. The effects of infill

walls may be accounted for by imposing the loads of the walls on to the beams on which

they rest. This idealization appears (or assumed?) to be adequate for analyzing the

building frame under static gravity loading neglecting the contribution of infills to the

stiffness of structure.

When the infill panel is connected to the frame the total system acts as a

sing1e unit. These infill walls, though constructed as secondary structural elements,

behave as a constituent part of the structural system and determine the overall behaviour

of the structure, especially when it is subjected to seismic loads. However, designers tend

to treat these infill walls as “non-structural” and treat the frames as conventional frames, a

practice that is far from representing the true behaviour.

A plastic model proposed in GANZ(1985) (Figure 3. 3) was recommended by M. Leipold

(2009), which consider such multiple damage modes. This model uses a combination of

yielding surfaces, where each surface captures one failure mode. Table 2 shows these

failure surfaces in detail. The failure modes are: tensile failure of the bricks (I),

compression failure of the bricks (II), shear failure of the bricks (III), sliding along the

mortar beds (IV) and tensile failure in the mortar beds (V). Only four independent input

parameters are needed to define the material law, the strength in the main directions, the

internal friction angle and the cohesion in the mortar beds.

P.G. Asteris (1980) quoted that in spite of broad application and

economical significance of infills, this structural system has resisted analytical modeling;

the following reasons may explain this situation:

Computational complexity: The particulate infill material and the ever-changing

contact conditions along its interface to concrete constitute additional sources of

Non-linear Dynamic analysis of Soil Structure Interaction of Three Dimensional Structure For Varied Soil conditions

Chapter III

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61

analytical burden. The real composite behavior of an infilled frame is a complex

statically indeterminate problem according to Smith (Smith 1966).

Structural uncertainities: The mechanical properties of masonry, as well as its

wedging conditions against the internal surface of the frame, depend strongly on local

construction conditions.

Non-linearity: The non-linear behavior of infilled frames depends on the separation

of masonry infill panel from the surrounding frame.

In the proposed approach, the infill is accounted for in the static as four nodded two

dimensional plane stress element. In dynamic analysis the infilled frame is idealized

either as a frame-diagonal strut system or as four nodded two dimensional plane stress

element depending on the diagonal distance after application of load increment.

When a lateral load is applied, the infill and the frame are getting separated over a large part of

the length of each side, and contact remains only adjacent to the corners at the ends of the

compression diagonal. The only accepted “natural” conditions between the infill and the frame are

either the contact or the separation condition. for which proposed finite element procedure is

implemented in following steps:

1. Initially each infill surrounded by frame elements on four sides is idealized as

plane stress element with four nodes and eight degrees of freedom.

2. After the first iteration Compute the nodal forces, displacements, and the stresses

at the corner points of the elements.

3. If the inclined distance between two opposite corners is less than the original

distance then the plane stress element is replaced by diagonal strut connecting the

corner. (Refer figure3. 3.)

3.2.2. Modelling of soil media

Soils are complex material consisting of a solid skeleton of grains in contact with each

other and voids filled with gas (air) and /or water or other fluid. The soil Skelton

transmits normal and shear forces at the grain contacts, and this Skelton of grains behaves

Non-linear Dynamic analysis of Soil Structure Interaction of Three Dimensional Structure For Varied Soil conditions

Chapter III

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62

in a very complex manner that depends on a large number of factors, void ratio and

confining pressure being among the most important. However, the overall behavior of the

soil skeleton may be captured within principles of continuum mechanics (solid

mechanics). Interspersed in the void is water (incompressible fluid) and gas (compressible

fluid), each of which obeys its own physical laws. The mixture of grains, water, and air

produces a material that, in comparison with other engineering materials, is one of the

most difficult to characterize.

Since the philosophy of foundation design is to spread the load of the structure on to the

soil, ideal foundation modeling is that wherein the distribution of contact pressure is

simulated in a more realistic manner. The variation of pressure distribution depends on

the foundation behaviour (viz., rigid or flexible: two extreme situations) and nature of soil

deposit (clay or sand etc.). However, the mechanical behaviour of subsoil appears to be

utterly erratic and complex and it seems to be impossible to establish any mathematical

law that would conform to actual observation. In this context, simplicity of models, many

a time, becomes a prime consideration and they often yield reasonable results. Attempts

have been made by researchers to improve upon these models by some suitable

modifications to simulate the behaviour of soil more closely from physical standpoint.

With the development of numerical methods such as finite element and finite difference

methods it has become feasible to analyze and predict the behavior of complex soil

structure and soil/structure interaction problems. Such analyses depend considerably on

the representation of the relations between stresses and strains for the various materials

involved in the geotechnical structure. In numerical computation the relations between

stresses and strains in a given material are represented by constitutive model, consisting

of mathematical expressions that model the behavior of the soil in a single element,

determine the deformations and the possibility of failure of the structure. And it is

therefore important to characterize these materials accurately over the entire range of

stresses and strains to which they will become exposed. Thus, the purpose of a

constitutive model is to simulate the soil behavior with sufficient accuracy under all

loading conditions in the numerical computations.

Keeping the above points and the objectives of research in view and duly

considering the method of analysis, the soil is modeled with linear and non-linear

Non-linear Dynamic analysis of Soil Structure Interaction of Three Dimensional Structure For Varied Soil conditions

Chapter III

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63

constitutive relations. In the present chapter finite element model is derived for linear

constitutive relations of soil. Non-linear model for soil and its development is discussed

in detail in chapter IV. In both cases soil is dicretized as brick element with eight nodes

having three degrees of freedom per node.

3.3. Finite element modelling

The solution of the problem of building frame-foundation beam-soil mass interaction

system needs a proper physical modeling and numerical analysis to access the more

realistic and accurate structural behaviour of the composite system. The powerful

numerical tool like finite element method can be used to analyze the problem considering

the superstructure, foundation and the soil mass to act as single integral compatible

structural unit. The material nonlinearity involved in the problem of soil structure-

interaction also needs a special numerical treatment. The discretization of the domain of

interaction system needs variety of isoparametric elements with different degrees of

freedom.

3.3.1 Types of elements

For the interaction of finite element static or dynamic analysis of a three dimensional

rigid jointed framed structure resting on soil, the following types of elements have been

adopted.

1) Columns and beams modelled as one dimensional element with six degrees of

freedom per node (three translational and three rotational dof).

2) In filled walls modelled as plane stress element with two translational degrees of

freedom per node.

3) Mat Foundation is modelled as plate element with five degrees of freedom per

node (three translational and two rotational degrees of freedoms).

4) Soil elements are modelled as eight noded brick element with three translational

degrees of freedom per node.

3.3.2 Stiffness matrix of beam element:-

A typical beam/ column element of the structure is shown in figure 3.5. In local co-

Non-linear Dynamic analysis of Soil Structure Interaction of Three Dimensional Structure For Varied Soil conditions

Chapter III

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ordinates the stiffness matrix of the beam element is given below

Where,

A – is the area of cross section of the beam element

E A – is Axial rigidity

E Iy – is Flexural rigidity about y-axis

E Iz – is Flexural rigidity about z-axis

G Jx – is Torsional rigidity

L – Length of the beam element

The stiffness of beam element is given by

Where T is transformation matrix and k stiffness matrix in local coordinates

)1.3(

40100

60

04

06

00

00000

06

012

00

6000

120

00000

20100

60

02

06

00

00000

06

012

00

6000

120

00000

20100

60

02

06

00

00000

06

012

00

6000

120

00000

40100

60

04

06

00

00000

06

012

00

6000

120

00000

2

3

23

23

2

3

23

23

2

3

23

23

2

3

23

23

L

EI

L

EIL

EI

L

EIL

GIL

EI

L

EIL

EI

L

EIL

EA

L

EI

L

EIL

EI

L

EIL

GIL

EI

L

EIL

EI

L

EIL

EAL

EI

L

EIL

EI

L

EIL

GIL

EI

L

EIL

EI

L

EIL

EA

L

EI

L

EIL

EI

L

EIL

GIL

EI

L

EIL

EI

L

EIL

EA

K

yx

yy

x

yy

xx

yx

yy

x

yy

xx

yx

yy

x

yy

xx

yx

yy

x

yy

xx

l

l

l

l

T

T

T

T

T

000

000

000

000

-----(3.3)

TkTK eTe)( ------(3.2)

Non-linear Dynamic analysis of Soil Structure Interaction of Three Dimensional Structure For Varied Soil conditions

Chapter III

65

65

)4.3(cos

22

22

22

22

22

22

yx

xyxzy

zx

xyx

zx

xyxzx

zx

xyx

zyx

l

CC

CosCSinCCSinCC

CC

CosCSinCC

CC

SinCCosCCCosCC

CC

SinCCCCCC

T

Where Cx , Cy and Cz are direction cosines of the beam with respect to global axes. is

the angle of twist of plane of symmetry of cross section with respect to x-y plane. The

element has been implemented in the three-dimensional finite element software and

checked against simple example 1., given in Rajashekharan et al (2000). Shown in figure

3.6.

3.3.3 Stiffness of Plane stress element

With the shape functions in terms of (r, s) co-ordinate system, the coordinates of any

point can be expressed in terms of (x, y) co-ordinates as

Where N =

In this case since the number of nodes are 4, n=4

dvBCk

bygiveniselementanof[k]t

B

matrixStiffness

-------

(3.7)

Where

[B], is strain displacement matrix

i

n

nii usrNsru ),(),(

i

n

nii vsrNsrv ),(),(

i

n

nii xsrNsrx ),(),(

i

n

nii ysrNsry ),(),(

-----(3.5)

------(3.6)4

)1)(1( ssrr ii

Non-linear Dynamic analysis of Soil Structure Interaction of Three Dimensional Structure For Varied Soil conditions

Chapter III

66

66

[C], is constitutive matrix

------(3.8)

Where, t is the thickness of 2-d element.

If the coordinates are transferred to natural coordinates ),( sr we have

-------(3.9)

Where |J| is determinant of Jacobian matrix [J]

The constitutive matrix for a plane stress condition is given by following equation

100

01

01

1 2

EC -----(3.10)

The Jacobian matrix

The Jacobian matrix in terms of shape functions and nodal coordinates is given by

dsdJBtt

rBCk

dsdrJdydx

dydxBCk

dydx tBCk

t

t

Bt

B

[J]

][

*22

*21

*12

*111-

s

rJJ

JJ

s

r

y

x

y

xJ

s

r

y

x

s

y

s

xr

y

r

x

s

r

------(3.11)

----(3.12)

----(3.13)

Non-linear Dynamic analysis of Soil Structure Interaction of Three Dimensional Structure For Varied Soil conditions

Chapter III

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67

n

i i

n

i i

n

i i

n

i i

ys

xs

yr

xr

1

i

1

i

1

i

1

i

*N

*N

*N

*N

[J] ------(3.14)

The strain Displacement matrix-[B]

qB][

i

i

iiii

ii

ii

xy

y

x

v

u

s

NJ

r

NJ

s

NJ

r

NJ

s

NJ

r

NJo

os

NJ

r

NJ

v

u

xy

xo

ox

*12

*11

*22

*21

*22

*21

*12

*11

-----

(3.15)

Four point Gauss quadrature has been adopted for two dimensional integral to find

element stiffness matrix and the validity of the program is done by comparing the out put

with analysis of a cantilever plate (test example 2) shown in figure 3.8 given in “Finite

element analysis”, by Krishnamoorthy (1994).

3.3.4 Development of stiffness and mass matrix for Plate element

Plate elements are used model to foundation mat. In thin plate theory, the tranverse shear

deformations are neglected and deformation is completely described by a function w(x,z)

where w is lateral displacement perpendicular to the plate. If the effects of transverse

shear deformations are to be considered, it is important to include these deformation in

their rotational degrees of freedom of nodes. The isoparametric plate element used is four

nodded with five degrees of freedom T][iyθ

ixθiwiviu per node.

The displacements and rotations at any point may be expressed in terms of shape

functions.

;

:;

4

1

4

1

4

1

4

1

4

1

iiziz

iixix

iii

iii

iii

NN

wNwvNvuNu

-----(3.16)

Non-linear Dynamic analysis of Soil Structure Interaction of Three Dimensional Structure For Varied Soil conditions

Chapter III

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68

The displacement vector is given by

Tiiuq ]v w[}{

iyxii

The stress resultants are given by

The strain vector is given by

Tzxxzzxxzzx

In the present work Mindlin;s theory is used to include shear deformation in plates.The

isoparametric plate element can allow the deformation due to transverse shear. Hence the

rotations zand x can be expressed as

where zand x are average shear rotations mid surface normal.

The constitutive relation for a plate element restrained against warping is given by

-----(3.17)

---(3.19)

-and- xx

vz

x

vzx

---(3.20)

-----(3.18) Tzxxzzxxzzx QQMMM

10

01

12

0

2

100

01

01

1(

2

100

01

01

1

0

0

)2

2

21

2

1

Eh

000

000

00

0

00

12

Eh

C

EC

C

C

3

---(3.21)

---(3.22)

----(3.23)

Non-linear Dynamic analysis of Soil Structure Interaction of Three Dimensional Structure For Varied Soil conditions

Chapter III

69

69

10

01

12

0

2

100

01

01

1(

2

100

01

01

1

0

0

)2

2

21

2

1

Eh

000

000

00

0

00

12

Eh

C

EC

C

C

3

---(3.21)

---(3.22)

----(3.23)

2221

1211 qBB

BB

qB

---(3.24)

(3.26)---

000

000

000

B

0

00

00

-(3.25)---

0

00

00

1211

1211

x

N

z

Nz

Nx

N

B

w

v

u

BB

xw

zu

zw

xu

ii

i

i

z

xxz

z

x

Non-linear Dynamic analysis of Soil Structure Interaction of Three Dimensional Structure For Varied Soil conditions

Chapter III

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70

(3.28)-------

000

000

000

B

0

00

00

(3.27)-----

0

00

00

1211

1211

x

N

z

Nz

Nx

N

B

w

v

u

BB

xw

zu

zw

xu

ii

i

i

z

xxz

z

x

The strain displacements is given by

The stiffness matrix of plate element is given by

ddJBtt

BCk . ----(3.30)

The element has been implemented in analysing a square plate having thickness/span

ratio of 0.2 and subjected to uniformly distributed load (test example 3) shown in figure

3.10 given in “Finite element analysis”, by Krishnamoorthy (1994).

3.3.5 Development of stiffness matrix for Brick element

The shape functions of a Hexahedral in natural coordinates are as follows:

-------(3.31)8---1,2,-ifor8

)1)(1)(1(

iii

i

ttssrrN

(3.29)------

0

0

0

0

B

00

00

000

000

000

2221

i

i

ii

i

i

i

i

N

Nx

N

z

Nz

Nx

N

x

Nx

NB

Non-linear Dynamic analysis of Soil Structure Interaction of Three Dimensional Structure For Varied Soil conditions

Chapter III

71

71

Where r, s, t are natural coordinates and ri,, si and ti are values of natural

coordinates for i. Refer figure 3.11

freedomofdegreesnodal theiswhere

8

1

1

1

8

1i

8

1i

8

1i

QB

zuxwywzv

xvyuzwyvxu

wvuQ

QN

w

wv

u

N

wN

vN

uN

w

v

u

xz

yz

xy

z

y

x

Tiii

ii

ii

ii

821Bismatrixntdisplacemestrain thewhere BBB

The derivatives of [B] is obtained by chain rule

x

N

z

Ny

N

z

Nx

N

y

Nz

Ny

Nx

N

B

ii

ii

ii

i

i

i

i

0

0

0

00

00

00

---(3.32)

---(3.33)

---(3.34)

---(3.35)

--(3.36)

Consider

zN

yN

xN

J

zN

yN

xN

tztytx

szsysx

rzryrx

tN

sN

rN

i

i

i

i

i

i

i

i

i

Non-linear Dynamic analysis of Soil Structure Interaction of Three Dimensional Structure For Varied Soil conditions

Chapter III

72

72

The stiffness matrix is obtained by using the formula]

k= dtdsdrJBCB t ******

The element has been implemented in the three-dimensional finite element software and

checked against simple example 4, given in “Introduction to Finite elements in

engineering” by Tirupathi R Chandra patla and Ashok, as shown in figure 3.12.

3.4. Development of soft ware

The development of computer technology has provided powerful support for SSI analysis

and thus computing has become an indispensable tool. The common analysis programs

include CLASSI, FLUSH, ALUSH, SASSI and HASSI have conspicuous disadvantages

in that they only analyzes in frequency domain and are incapable of nonlinear analysis. At

present there are a large number of available commercial finite element programs (such as

ANSYS, ABAQUS, MSC.MARC), which have friendly inter- face and powerful

nonlinear solver. They process well and are easy to master for users with great generality

and therefore are very popular among SSI studies. When applying them to study SSSI, the

biggest problem lies in how to solve the huge calculation amount brought by the large

range of soil. But are incapable of handling when problems arise that are beyond the

----(3.40)

1,8i

11

11

11

Jwhere

bygivenisandMatrixJacobian theis[J]Where

81

81

81

1

8

1

8

1

8

1

8

1

8

1

8

1

8

1

8

1

8

1

iiii

iiii

iiii

i

i

i

i

i

i

ii

i

ii

i

ii

i

ii

i

ii

i

ii

i

ii

i

ii

i

ii

i

ssrrttN

ttrrssN

ttssrrN

tN

sN

rN

J

zN

yN

xN

zt

Ny

t

Nx

t

N

zs

Ny

s

Nx

s

N

zr

Ny

r

Nx

r

N

tztytx

szsysx

rzryrx

-----(3.39)

----(3.38)

--(3.37)

Non-linear Dynamic analysis of Soil Structure Interaction of Three Dimensional Structure For Varied Soil conditions

Chapter III

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73

standard capability of the tool.

Since many individuals write programs for a broad range of applications, most high-level

computer languages, like FORTRAN and C, have rich capabilities. Although some

engineers might need to tap the full range of these capabilities, most merely require the

ability to perform engineering-oriented numerical calculations.

Finite element analysis is a method for numerical solution of field problems and a field

problem is the spatial distribution of one or more dependent variables. The region of

interest for the distribution of this field is mapped or geometrically defined by nodes and

than discretized into and represented by “finite” geometric units in which the field

variable is allowed to vary from node to node in a way described by a polynomial

function. The location of the nodes is the locations where the value of field of interest is

sought. The units, which are defined by “nodes”, are called the “elements”, and the

particular assembly of these elements is called the mesh. The algebraic equations within

these elements are solved for the unknown field quantities at the nodes.

The solution procedure for a time-independent FEA can be summarized as:

1. Description the element behavior through matrices.

2. Assembly of the individual matrices through element connection.

3. Establishing the loading and boundary conditions.

4. Determination of nodal quantities through algebraic equations created by a system of

structure matrix, loading and the boundary conditions.

5. Computation of gradients.

In the present research FORTRAN 77 is used to take following input for a Static SSI

analysis:

Young’s modulus and rigidity modulus, and unit weight of beam material,

Young’s modulus of soil at top and bottom, unit weight and poisons ratio of soil.

Young’s modulus, rigidity modulus, unit weight and poisons ratio of foundation

material.

Young’s modulus, unit weight and poisons ratio of infills material.

Non-linear Dynamic analysis of Soil Structure Interaction of Three Dimensional Structure For Varied Soil conditions

Chapter III

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74

Breadth, depth and load on beams in X-direction.

Breadth, depth and load on beams in Z-direction.

Breadth and depth of column.

Length, breadth and depth of mat/ isolated footings and Load on mat foundation.

Number of layers of soil in X, Y and Z directions.

Thickness of soil layers in X, Y and Z directions.

Number of plate elements (representing raft foundation or isolated footing) and

soil elements beyond column edge in X and Z directions towards boundary.

Number of plate elements (isolated footing) on either side of columns in X and Z

directions.

Number of columns in X and Z directions

Number of soil elements between columns in X and Z direction.

The matrix displacement equations are linear simultaneous equations. The features of

matrix displacement equations are as follows

i) The matrix is having diagonal dominance and is positive definite. Hence in

the solution process there is no need to rearrange the equations to get

diagonal dominance.

ii) The matrix is symmetric.

iii) The matrix is having banded nature i.e., the nonzero elements of stiffness

matrix are concentrated near the diagonal of the stiffness matrix.

Considerable saving can be achieved in memory of computers by avoiding

storage of zero values of stiffness matrix.

Since the size of stiffness matrix is very large it results in shortage of memory. Hence

optimizing memory requirement to store stiffness matrix values becomes essential. The

line separating the top zero elements from the first non – zero element is called the

Skyline. In this system of storage, if there are zero elements at the top of a column, only

the elements from the first non-zero value need to be stored. This method is called

Non-linear Dynamic analysis of Soil Structure Interaction of Three Dimensional Structure For Varied Soil conditions

Chapter III

75

75

Skyline storage and is used in the present work.

Contents of the global stiffness matrix before reduction is often has less than 5%

number of non-zero elements and perhaps less than 1% non-zero elements if there are

thousands of degrees of freedom. During reduction of stiffness a direct solver changes

most zeros between the skyline and diagonal to nonzero, but leaves zeroes above the

skyline intact, so the matrix remains sparse. A profile or skyline single array storage

scheme is adopted to save the memory space needed in the storage of the matrices. An

active column profile (skyline) solution algorithm is employed in the equation solution

module to solve the equations efficiently. The use of this method with an active column

profile storage scheme leads to a very compact program where it is very easy to use

vector dot product routines to effect the triangular decomposition and forward reduction.

This computational advantage is very important to modern computers which are vector

oriented. Therefore software exploit this sparcity by using compact storage formats, so

that nonzero elements are neither stored nor processed. Three subroutines COLUMNH,

CADNUM and PASSEM were developed for static analysis. The subroutines which are

developed in dynamic analysis are dealt in chapter---.

To accomplish the above steps, in the present research, FORTRAN 77 is used and

following subroutines are developed:

Subroutine Mesh Generates Finite element mesh, generates element noderelationship, coordinates of nodes, relationship betweenelement and Global degrees of freedom .

Subroutine Columh Calculates column height and size of compact columnmatrix.

Subroutine cadnum Gives the diagonal address of diagonal elements incompact column matrix.

Subroutine Passem Assembles compact column matrix from stiffness matrixof individual element..

Subroutine Brickstif Calculates stiffness matrix of brick element.

Subroutine Brickload Calculates the load vector due to self weight of soilelements

Subroutine Plate Calculates stiffness matrix of plate element

Subroutine Beamstif Calculates stiffness matrix of beam element element

Subroutine Wallstif Calculates stiffness matrix of wall element

Non-linear Dynamic analysis of Soil Structure Interaction of Three Dimensional Structure For Varied Soil conditions

Chapter III

76

76

Subroutine Frameload Calculates load vector from loads acting on the frame

Subroutine Plateload Calculates load vector from loads acting on the raft

Subroutine Passem Assembles compact column matrix from stiffness matrixof individual element

Subroutine Pasolv Solves the algebraic equations and calculatesdisplacement vector

Subroutine Brickstress Calculates stresses at Gauss points in brick element

Subroutine brickstress1 Calculates stresses at apex points in brick element

Subroutine brickstress2 Calculates stresses at centre of brick element

Subroutine Plateforces Calculates stress resultants in plate elements

Subroutine Wallstres Calculates stresses in two dimensional plane stresselement

Subroutine Beamforces Calculates stress resultants in beam elements in local co-ordinates

Subroutine Beamforces1 Calculates stress resultants in beam elements in Globalco-ordinates

Subroutine Trans Evaluates displacement transformation matrix for beamelement

Subroutine Hypo Evaluates constitutive matrix of Hypo-elastic model

Subroutine subpq Evaluates stress invariants in brick element.

3.5. Validation of FEM model and Coding.

Literatures on SSI problems for three dimensional structures are available for cases of

linear elastic structure and soil. Therefore, firstly, FEM model coding has been done for

the same by considering uniform young’s modulus for soil.

The structure under consideration is shown in figure 3.13 and the geometrical details are

given in table 3.1. This size is arrived after ascertaining negligibly small stresses at the

boundaries. For this three dimensional structure, the SSI analysis is carried out for both

the uncoupled and coupled cases of interface between the foundation and soil.

3.5.1. Finite element Formulation

The soil is modeled with 33 X 21 X 7 layers in longitudinal, Transverse and vertical

directions respectively resulting in 4851 hexahedron elements. The number of plate

Non-linear Dynamic analysis of Soil Structure Interaction of Three Dimensional Structure For Varied Soil conditions

Chapter III

77

77

elements for raft foundation is 135, the numbers of beam elements in longitudinal

Table 3.1

Sl no Structure Componenet Details

No. of storeys 5

No. of bays 5X3

Storey height 3.5m

Bay width 5m

Beam size 0.3X0.6m

Column size 0.4X0.4

1 Frame

Raft size 25.0X15.0X0.4

2 Soil Soil mass 153.0mX95.0mX20.0m

3 Elastic modulus of soil 1.33X107 N/m2

4 Poissons ratio of soil 0.45

5 Bulk modulus of concrete 6.1X106 N/m2

6 Elastic modulus of concrete 1.4X1010 N/m2

direction (X-direction) are 80, in transverse (Z-direction) are 72 and the number of

columns is 96. In the SSI analysis of Frame-Mat-Soil system (Figure 3.14) following

types of elements have been adopted:

a) Soil elements are modeled as eight noded brick element with three translational

degrees of freedom per node viz., D7, D2, and D8.

b) Mat Foundation is modeled as plate element with five degrees of freedom per

node three translational degrees of freedom (D1, D2, and D3) and two rotational

degrees of freedom (D4 and D5).

c) Columns and beams are modeled as one dimensional element with six degrees of

Non-linear Dynamic analysis of Soil Structure Interaction of Three Dimensional Structure For Varied Soil conditions

Chapter III

78

78

freedom per node (three translational and three rotational dof).

Figure 3.15 gives details of frame

3.5.2. Validation

The theoretical formulation and the program developed was validated with respect

to a Publication by king (1974) involving linear analysis for loads of 19.6 kN/m2 on raft,

15kN/m and 25kN/m on exterior and interior beams respectively. The details of structure

are given in Table 3.1.

The results obtained from the present model and the coding are found to be in good

agreement with the results of above mentioned published work. Validations of results are

obtained for paper published by king and Chandrashekharan involving linear analysis.

3.5.2.1. Comparison of settlements.

The settlement of the raft obtained from the present analysis in the proposed work and the

settlements obtained in the referred work done by Chandrashekharan (1974) and King

(1977).. There has been good comparability between the results. Figure 3.16 gives the

contours settlement below raft. In the referred papers authors have used 7 and 9 layers in

vertical and horizontal directions half the domain on either side. In the present analysis 33

X 21 X 7 layers longitudinal, transverse and vertical directions.

3.5.2.2. Comparison of contact pressure.

The distribution of contact pressure along longitudinal direction and

transverse direction are shown in figure 3.17 and 3.18. The values of pressure at various

points along sections are nearly matching with referred work.

Pressure distribution along axes of symmetry

The pressure at the ends is 1.4587 times the pressure at the centre according

to Chandrashekaran et al. In the present work it is found that pressure at ends is 1.4938

times pressure at centre. But in transverse direction pressure at ends is found to be 1.6654

times pressure at centre.

Maximum pressure occurred along a strip at Z/B= + 0.45 in longitudinal direction and

X/L= + 0.47 in transverse direction.

Non-linear Dynamic analysis of Soil Structure Interaction of Three Dimensional Structure For Varied Soil conditions

Chapter III

79

79

In Longitudinal direction, for X/L=+ 0.47, the vertical pressure at Z/B=+ 0.45 was

1.384 times the pressure at Z/B=+ 0.0

In Longitudinal direction, for X/L=0.0, the vertical pressure at Z/B=+ 0.45 was 1.665

times the pressure at Z/B=+ 0.0 .

In transverse direction, for Z/B=+ 0.45, the vertical pressure at X/L=+ 0.47 was 1.242

times the pressure at X/L=+ 0.0

In transverse direction, for Z/B=0.0, the vertical pressure at X/L=+ 0.47 was 1.49 times

the pressure at X/L=+ 0.0

Non-linear Dynamic analysis of Soil Structure Interaction of Three Dimensional Structure For Varied Soil conditions

Chapter III

Figure3.1:Modelling of a 3-D SSI problem

Figure 3.2: Models for RC Structural elements. (Courtesy: M.Leipold et al. 2009)

Figure 3.3 : Models for infills in RC frame. (Courtesy: M.Leipold et al. 2009)

and J. Schwarz

Figure 3.4: Equivalent strut element

Non-linear Dynamic analysis of Soil Structure Interaction of Three Dimensional Structure For Varied Soil conditions

Chapter III

Figure 3.7 Bilinear Rectangular element Isoparametriccoordinate mapping (a)

r

s

1r

1s

1r

1s

Fig(a) Fig

(b)

Figure 3.8: Test example 2 (Courtesy Krishnamoorthy,1994)

3 m

2kn/m

6 m

8 m

4 m

Figure 3.6: Test example 1 (Courtesy:Rajashekharan et al (2000))

u2

v2w2

2x

2y

v1w1

1x

1y1z

X

Y

Z

Y

x

y

z

xzy

Figure 3.5: Local and global co-ordinate of the Euler-Bernoulli beam element.

Non-linear Dynamic analysis of Soil Structure Interaction of Three Dimensional Structure For Varied Soil conditions

Chapter III

MxZ*

Qx*QZ

*MZx*

MxZ MZx

XZ

Y

Qx QZ

MZ*

Figure 3.10: Test example 3

3 7 1115

4 8 1216

2 6 1014

1 5 913

1718

20 19X

Y

Z

100 mm

100 mm

100 mm 100 mm 100 mm

80 KN

Figure 3.12: Test example 4, Cantilever beam.

8 (-1,1,1)

5 (-1,-1,1)6 (1,-1,1)

2(1,-1,-1)

3 (1,1,-1)

4 (-1,1,-1)

7 (1,1,1)

1 (-1,-1,-1)

r

tr

sr

Non-linear Dynamic analysis of Soil Structure Interaction of Three Dimensional Structure For Varied Soil conditions

Chapter III

D5

D2

D3

D4

D1

D6

D7D2

D8

D1

D2

D3

D4D5

Fig 1(a)

Fig 1(b) Fig 1(d)

Fig 1(c)

Figure3.13 . Details of the model and elements used

X (Longitudinaldirection)

Plan

Figure 3.14 Details of fem model for frame- raft-soil interaction analysis

Z ( Transversedirection)

L

B

X (Longitudinaldirection)

Y (Verticaldirection)

Raft discretization

A B

AC

A

2

A1

A

Elevation

Z ( Transversedirection)

Non-linear Dynamic analysis of Soil Structure Interaction of Three Dimensional Structure For Varied Soil conditions

Chapter III

1A A

BA

CA

2A

5m5m

5m5m

5m5m

5m

5m

5m

3.5 m

3.5 m

3.5 m

3.5 m

A BA

CA

2A

1A

171,172,173

153,187153,177

81,93

84,96

87,99

88,102

153,154,155

159,160,161

165,166,167

177,178,179

183,184,185

189,190,191

195,196,197

82,94

85,97

88,100

89,103

154,188154,188

1, 21, 2, 22 3, 33

6, 26 7, 27 8, 28

11, 31 12, 32 13, 33

16, 36 17, 37 18, 38

155,189

159,183

160,184

161,185

165,189

166,190

167,191

171,196

172,197

173,198

154,178

155,179

Figure 3.15: Details of frame

Non-linear Dynamic analysis of Soil Structure Interaction of Three Dimensional Structure For Varied Soil conditions

Chapter III

-0.5 -0.44 -0.36 -0.3 -0.24 -0.16 -0.1 -0.04 0.04 0.1 0.16 0.24 0.3 0.36 0.44 0.5-0.5

-0.4

-0.267

-0.167

-0.067

0.067

0.167

0.267

0.4

0.5

-0.5

-0.2

4

0.04 0.3

S1

S4

S7

S10

-50--49.75 -49.75--49.5 -49.5--49.25 -49.25--49 -49--48.75 -48.75--48.5-48.5--48.25 -48.25--48 -48--47.75 -47.75--47.5 -47.5--47.25 -47.25--47-47--46.75 -46.75--46.5 -46.5--46.25 -46.25--46 -46--45.75 -45.75--45.5-45.5--45.25 -45.25--45 -45--44.75 -44.75--44.5 -44.5--44.25 -44.25--44-44--43.75 -43.75--43.5 -43.5--43.25 -43.25--43 -43--42.75 -42.75--42.5-42.5--42.25 -42.25--42 -42--41.75 -41.75--41.5 -41.5--41.25 -41.25--41-41--40.75 -40.75--40.5 -40.5--40.25 -40.25--40 -40--39.75 -39.75--39.5-39.5--39.25 -39.25--39 -39--38.75 -38.75--38.5 -38.5--38.25 -38.25--38-38--37.75 -37.75--37.5 -37.5--37.25 -37.25--37 -37--36.75 -36.75--36.5-36.5--36.25 -36.25--36 -36--35.75 -35.75--35.5 -35.5--35.25 -35.25--35-35--34.75 -34.75--34.5 -34.5--34.25 -34.25--34 -34--33.75 -33.75--33.5-33.5--33.25 -33.25--33 -33--32.75 -32.75--32.5 -32.5--32.25 -32.25--32-32--31.75 -31.75--31.5 -31.5--31.25 -31.25--31 -31--30.75 -30.75--30.5-30.5--30.25 -30.25--30 -30--29.75 -29.75--29.5 -29.5--29.25 -29.25--29-29--28.75 -28.75--28.5 -28.5--28.25 -28.25--28 -28--27.75 -27.75--27.5-27.5--27.25 -27.25--27 -27--26.75 -26.75--26.5 -26.5--26.25 -26.25--26-26--25.75 -25.75--25.5 -25.5--25.25 -25.25--25 -25--24.75 -24.75--24.5-24.5--24.25 -24.25--24

Figure 3.15: Vertical Displacement contours below raft foundation

-0.15

-0.1

-0.05

0-0.55 -0.45 -0.35 -0.25 -0.15 -0.05 0.05 0.15 0.25 0.35 0.45 0.55

V e

r t

I c

a l

s t

r e

s s

(M

Pa)

0.55 0.45 0.33 0.216 0.116 0.0

``

-0.15

-0.1

-0.05

0-0.55 -0.45 -0.35 -0.25 -0.15 -0.05 0.05 0.15 0.25 0.35 0.45 0.55

V e

r t ic

a l

s r

e s

s (M

Pa)

0.53 0.47 0.4 0.33 0.27 0.2 0.13 0.07 0.0

Figure 3.16: Vertical stress along longitudinal section fordifferent values of h

Figure 3.17: Vertical stress along tranverse direction fordifferent values of x


Recommended