Numerical model of three-dimensional coupled wall structures.
Miedzialowski, Czeslaw ; Chyzy, Tadeusz ; Kretowska, Joanna 等
Abstract. Three-dimensional description of a building structure
taking into consideration the soil structure interaction is a very
complex problem; the solution of it is often obtained by the
finite-element method. However, this method takes a significant amount
of computational time and memory. Therefore an efficient computational
model based on the subdivision of the structure into building elements
such as wall and floor slab elements, plane and three-dimensional joints
and lintels, that could provide accurate results with a significantly
reduced computational time, is proposed in this study for the analysis
of three-dimensional structures. The examples prove the efficiency and
the computing possibilities of the model.
Keywords: three-dimensional building elements, super elements,
dynamic problem formulation, finite-element method.
1. Introduction
Three-dimensional description of building structure taking into
consideration soil structure interaction is a very complex problem and
solution of this problem is often obtained by the finite element method.
The building structure and the subsoil create a uniformly interacting
system which can be accurately described only by three-dimensional
analysis. Such analysis allows not only to design building structures in
an efficient way but also to take into account complicate load and soil
conditions Fig 1. On the area of Poland, the kinematic loads are caused
mostly by mining [1] and road traffic (paraseismic effects), but lately
the typical seismic effects have been noticed in north-eastern part of
Poland and Lithuania.
[FIGURE 1 OMITTED]
The computational model created to solve these problems, which uses
classical finite elements, incorporates substantial disadvantages as a
result of high time-consuming computations (a high number of degrees of
freedom) and extended data processing.
Many building structures are constructed using coupled shear walls
or shear wall-frame systems. Therefore much research on efficient
analysis of such structures has been undertaken [2-4]. Plane stress
elements and beam elements have been used to model the shear wall core
and frames. The transition region in which beam and shear walls or
frames are interconnected is often the weakest area. In general, wall
element is treated in FEM as plane stress element (has two translational
degrees of freedom per node) and beam element has three degrees of
freedom per node (two translational and one rotational). Due to this
reason, many research workers have taken into account the connections
between shear wall and beam or shear wall and frame [4-7].
The paper presents an efficient three-dimensional computational
model (called MQDES) based on subdivision of the structure into building
elements such as wall and floor slab elements, plane and
three-dimensional joints and lintels, that could provide accurate
results with significantly reduced computational time. The theory of
Timoshenko-type beam has been used to describe wall and floor strips but
the compression and twisting have been added to the classical
formulation. The description allows to obtain internal forces for every
strip what can be very useful in the engineering practice (designing
process).
Proposed model can be useful for the analysis of three-dimensional
structures subjected to dynamic and static loads but especially for the
analysis of building structures, where mainly walls are responsible for
the stiffness of the building.
2. The computational model
2.1. The model formulation
The computational model is formulated on the basis of the finite
element method in agreement with Zienkiewicz [8]. The discrete model is
constructed using the subdivision of the structure into building
elements such as wall and floor slab elements, plane and
three-dimensional joints (vertical and horizontal) and lintels [9] (Fig
2).
[FIGURE 2 OMITTED]
Wall and floor elements (Fig 3a), which are treated as vertical and
horizontal strips, are described by deep beam scheme taking into account
compression and twisting. Transverse section deformation is assumed as
in Thimoshenko-type beam in agreement with [10].
[FIGURE 3 OMITTED]
The displacement field of wall and floor strips is expressed by
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII.], (1)
where: [phi]--angle of rotation of the strip cross-section,
[psi]--angle of twist of the strip cross-section.
The strain field is written as
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII.], (2)
where: l, p--two adjacent points between which strain is averaged,
L--distance between points l and p (width of the strip).
The strain vector has the form
[[epsilon].sub.w] = L[bar.f]w, (3)
where:
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII.] (4)
[bar.f]w = [{[u.sub.l] [u.sub.p] [w.sub.0] [phi] [psi]}.sup.T] (5)
The stress field is determined as follows:
[sigma] = D[epsilon] = DL[bar.f]w, (6)
where: D--constitutive matrix.
Plane and spatial joints are placed between floor and wall strips.
The displacement field in the plane joints (Fig 3c) can be
expressed by:
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII.]. (7)
The strains can be calculated as follows:
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII.], (8)
where:
[[epsilon].sub.x] = ([u.sub.l] - [u.sub.p])/[l.sub.l], (9)
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII.], (10)
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII.], (11)
where: [[phi].sub.r]--angle of rotation of the plane joint
cross-section, [[psi].sub.r]--angle of twist of the plane joint
cross-section, [l.sub.n]--width of the joint.
Connection between 3 or 4 strips and 2 strips situated in a
different plane is described by three-dimensional joint (Fig 3d, e).
However, the displacement field of the spatial joints (Fig 3d) is
assumed as in three-dimensional state of stress.
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII.]. (12)
Strain field is calculated as
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII.]. (13)
Stress field can be described by
[[sigma].sub.j] = D[[epsilon].sub.j] = D[L.sub.j][f.sub.j], (14)
where:
D = [E.sub.j]/(1 + v) (1 - 2v) ([D.sub.diag] + [D.sub.12]), (15)
[D.sub.diag] = [1 - v, 1 - v, 1 - v, 1 - 2v/2, 1 - 2v/2, 1 - 2v/2],
(16)
[D.sub.12]--matrix 6 x 6, in which: [D.sub.12] = [D.sub.13] =
[D.sub.21] = [D.sub.23] = [D.sub.31] = [D.sub.32] = v; the other
elements are equal 0.
2.2. The finite element method application
The problem solution using the finite element method is reduced to
a defined number of points, called nodes.
The unknown displacements distribution of wall and floor elements
[[bar.f].sub.w] is expressed by:
[[bar.f].sub.w] = N[d.sub.e], (17)
where N--shape function matrix, [d.sub.e]--vector of unknown
displacements at nodes of finite elements
[d.sub.e] = [{[u.sup.i.sub.l], [u.sup.i.sub.p], [w.sup.i],
[[phi].sup.i], [[psi].sup.i], [u.sup.k.sub.l], [u.sup.k.sub.p],
[w.sup.k], [[phi].sup.k], [[psi].sup.k]}.sup.T] (18)
The equation of virtual work in dynamic problem is given by
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII.], (19)
where: c--damping parameter, [rho]--mass parameter, p(t)--changing
load.
The equation (20), expressed by internal forces W, has been
obtained by formulas (3) and (4) and by integration of the equation (19)
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII.], (20)
where F-cross-sectional area.
W = {[N.sub.x], [N.sub.z], [Q.sub.zx], [M.sub.y], [M.sub.s]}. (21)
Internal forces can be obtained by using FEM
W = [bar.D]L[bar.f] = [bar.D]LN[d.sub.e] = [bar.D]B[d.sub.e], (22)
where: [bar.D]--constitutive matrix, N--matrix of a shape function,
[d.sub.e]--displacement vector of nodes.
Using equation (20) the typical system of differential equations
can be obtained
M[??] + C[??] + Kd = P(t). (23)
The solution of the equation (26) can be obtained by using one of
well-known numerical method, ie indirect method (reduction and modal superposition) or direct method (Newmark and finite difference method).
In order to enable easier implementation of connections of finite
elements, according to the presented model, the unknown displacements
are transferred to the corners of elements (Fig 3b).
2.3. Soil-structure interaction problem
The subsoil is presented as elastic contact model described by
spring constraints (Fig 4).
[FIGURE 4 OMITTED]
Taking into account structural elements, the displacements can be
expressed as follows [11]:
[u.sub.1] = [u.sub.1], (24)
[u.sub.p] = [u.sub.2], (25)
w = [w.sub.1] + [w.sub.2]/2, (26)
[phi] = [w.sub.1] - [w.sub.2]/L, (27)
[psi] = [v.sub.1] - [v.sub.2]/L. (28)
The forces of subsoil interaction have the form:
[K.sub.f] [d.sub.f] = [R.sub.f], (29)
where:
[K.sub.f] = [K.sub.f diag] + [K.sub.f 12], (30)
[K.sub.f diag] = [a [b.sub.1] -c a [b.sub.1] -c], (31)
[d.sub.f] = [{[u.sub.1], [w.sub.1], [v.sub.1], [u.sub.2],
[w.sub.2], [v.sub.2]}.sup.T], (32)
[R.sub.f] = [{[R.sub.[u.sub.1]], [R.sub.[w.sub.1]],
[R.sub.[v.sub.1]], [R.sub.[u.sub.2]], [R.sub.[w.sub.2]],
[R.sub.[v.sub.2]]}.sup.T], (33)
where: [R.sub.f]--forces of subsoil interaction, [K.sub.f
12]--matrix 6x6 in which: [k.sub.25] = [k.sub.52] = [b.sub.2],
[k.sub.36] = [k.sub.63] = c and the other elements equal 0.
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII.]. (34)
[F.sub.f], [J.sub.f], [J.sub.0]--cross-sectional area and moments
of inertia of the foundation footing, [k.sub.u], [k.sub.v],
[k.sub.w]--proportional subsoil coefficients [12].
Taking into account the subsoil, the computational model has a
form:
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII.], (35)
where: k--degree of freedom of the structure, f--degree of freedom
of the contact zone between structure and subsoil.
2.4. The model loads
In case of problems changeable with time the system of differential
equations (23), (25) is to be solved.
The equation of motion for kinematic loads transferred from subsoil
to building structure has the form:
M([??] + [[??].sub.g]) + C[??] + Kd = 0, (36)
where: M--inertia matrix, C--damping matrix.
In case of "step by step" method of integration the C
matrix is often exchanged by combination of inertia-stiffness damping:
C = [alpha] x M + [beta] x K, (37)
[alpha], [beta]--coefficients, K--stiffness matrix,
[??]--acceleration vector, [??]--velocity vector, d--displacement
vector, g [[??].sub.g]--equivalent acceleration vector of vibrations
transferred from subsoil to building structure.
[[??].sub.g] = [summation over (i)] [a.sup.i.sub.g] x [T.sub.i],
(38)
[T.sub.i]--transformation vector for i-direction of vibration,
[a.sup.i.sub.g] - i--component of building footing acceleration.
Because the acceleration components [a.sup.i.sub.g] are known from
recorded vibration accelerograms, the equation (36) has now the form:
M[??] + C[??] + Kd = -M[[??].sub.g] = P(t). (39)
3. Numerical tests
The numerical tests present the verification of the correctness,
accuracy and efficiency of the proposed computational model by
comparison with the results obtained by using classic finite elements.
The correctness of the presented elements has been estimated according
to the principals used in FEM [8]. Both described in the paper new
elements and classic finite elements have been implemented into the
author's software "ORCAN"
(kmb.pb.bialystok.pl/dydaktyka/tchyzy).
The dynamic response of the building models have been tested under
paraseismic impact load. The results have been compared taking into
account displacements and computational time.
3.1. Numerical test No 1
Test No 1 concerns the single segment of the 11-storey building
(large-panel building technology). Concrete of B-20 class (according to
Polish standards and C16/20 according to EC2) has been used for walls
and floors of 14 cm thickness. Fig 5 a shows the horizontal projection of the segment, Fig 5 b--the computer model of the building which
consist of elements proposed in the paper. The dynamic response of the
building model has been tested under paraseismic impact load which had
been registered on mining area of industrial complex KGHM "Polska
Miedz" in Polkowice (Poland). Fig 6 shows the accelerogram. The
kinematic load used in the analysis corresponds to the results obtained
from the measurements of the building foundation. The load direction is
in Y axis (Fig 5).
[FIGURES 5-6 OMITTED]
The computations have been carried out by using the author's
software "ORCAN".
Figs 7 and 8 present the analysis results:
* MQDES(H)--analysis has been carried out by using
"ORCAN" and elements presented in the paper. System
discretisation correspond to the natural division of the building
structure into wall and floor elements.
* ORCAN--analysis has been carried out by using "ORCAN"
with 4-node shield elements and 4-node plane elements. The results have
been obtained by concentration of mesh 1, 2 and 4 times in both plane
directions what correspond to the division into 1, 4 and 16 elements in
comparison with the natural division into wall or floor elements.
[FIGURES 7-8 OMITTED]
Fig 7 shows the response in the form of displacements w of segment
top (without damping). Fig 8 presents the response in the form of
displacements v of segment top (without damping). The denotations
ORKAN-1, -2, -4 concern the mesh concentration by using classic
shield-plate finite elements what correspond with the division into 1, 4
and 16 elements in comparison with the natural division into wall or
floor elements.
Table 1 presents computational times of the analysis, where:
* Newmark method has been used for the integration if motion
equations and the elements stiffness matrices have been determined in
every time step,
* damping has been omitted,
* number of integration steps NSTEP = 1500,
* shield-plate elements have been integrated numerically: Gauss
points number-3x3, number of degree of freedom--20.
This test shows that proposed model which used MQDES elements can
well describe dynamic response of the building and can provide accurate
results with significantly reduced computational time.
3.2. Numerical test No 2
Fig 9 shows the 4-storey building erected in the same technology as
structure in test No 1. The building consists of 3 identical segments.
[FIGURE 9 OMITTED]
The dynamic response of the building has been tested under
paraseismic impact load showed in Fig 9. The load direction is in Y axis
(Fig 9). Fig 10 presents the response in the form of displacements w of
segment top (without damping). Fig 11 shows the response in the form of
displacements v of segment top. The denotations ORKAN-1, -2 concern the
mesh concentration by using classic shield-plate finite elements what
correspond with the division into 1 and 4 elements in comparison with
the natural division into wall or floor elements.
[FIGURES 10-11 OMITTED]
Table 2 presents computational times of the analysis, where:
* Newmark method has been used for the integration of motion
equations, and the elements stiffness matrices have been determined in
every time step,
* damping has been omitted,
* number of integration steps NSTEP = 5000,
* shield-plate elements have been integrated numerically: Gauss
points number-3x3, number of degree of freedom--20.
This test proved that proposed model which used MQDES elements can
well describe dynamic response of the building and can provide accurate
results with significantly reduced computational time.
3.3. Example of practical application
Computational example No 3 shows the real application of the
presented model--the results of the dynamic computations of the building
located in the mining area.
Fig 12 presents the building erected in WWT technology. The
building consists of 7 habitation segments and 4 separated staircases
(KL).
[FIGURE 12 OMITTED]
The staircases are the subject of the analysis. Building has been
subjected to kinematic load in the form of subsoil vibrations on the
mining area Fig 13 b). In Fig 14 the eigenvalues and their vibration
forms have been presented.
[FIGURES 13-14 OMITTED]
Fig 15 shows the horizontal displacements diagrams, where P4, P8
and P11 are the displacements appropriately at the level of 4, 8 and 11
ceiling.
[FIGURE 15 OMITTED]
4. Conclusions
The presented method opens possibilities for the modelling and
discretisation of complex three-dimensional building structures. The
model is assembled of elements corresponding to the division of a real
structure into constituent elements, i e wall panels, floor slabs, plane
and spatial joints as well as lintels. The description of stiffness
changes, which is determined at the level of the individual
cross-sectional areas of the building elements, does not increase the
number of unknowns. Such a modelling and description of stiffness
changes allow to create a computational model with a comparatively small
number of unknowns.
Because of the small number of unknowns the dynamic analysis of
large building structures in three-dimensional scheme can be carried out
easily in relatively short time on commonly used hardware of PC class
(the computational time is from dozens to several-hundreds times less in
comparison with the commercial software).
Numerical tests have confirmed the correctness and usefulness of
the presented method for the analysis of complex structures subjected to
kinematic load.
This model can be very useful for scientific research and code
verification purposes, for testing simple computational models, for
structural designing in complicated load and soil conditions, for
carrying out expertises or for modernisation existing building systems.
Received 26 July 2005; accepted 26 May 2006
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[8.] ZIENKIEWICZ, O. C. The finite element method. McGraw-Hill,
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[11.] MIEDZIALOWSKI, Cz. Discrete model of complex
three-dimensional structural schemes of buildings taking into account
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ERDVINIU PASTATU SKAITINIS MODELIAVIMAS
Cz. Miedzialowski, T. Chyzy, J. Kretowska
Santrauka
Trimacio pastato modelio analize, ivertinant statinio ir grunto
saveika, yra labai sudetingas uzdavinys. Jis sprendziamas taikant
baigtiniu elementu metoda. Taciau, tiesiogiai taikant si metoda, reikia
didelio kompiuterio pajegumo bei laiko sanaudu. Todel pasiulytas
hierarchinis skaiciuojamasis modelis sioms trimatems problemoms spresti.
Siame modelyje pastatas dalijamas i statybinius elementus, tokius kaip
sienu ir perdangu plokstes, dvimaciai bei trimaciai mazgai, saramos.
Taikant si modeli, gaunami tikslus rezultatai, kartu gerokai
sutrumpinamas skaiciavimo laikas. Pateikti pavyzdziai iliustruoja
pasiulyto modelio galimybes bei efektyvuma.
Reiksminiai zodziai: trimaciai pastatu elementai, superelementai,
dinamine uzdavinio formuluote, baigtiniu elementu metodas.
Czeslaw Miedzialowski (1), Tadeusz Chyzy (2), Joanna Kretowska (3)
Institute of Civil Engineering, Bialystok Technical University, ul.
Wiejska 45E, 15-351 Bialystok, Poland. E-mail: (1)
Cz.Miedzialowski@kmb.pb.bialystok.pl; (2) teddy@ pb.bialystok.pl; (3)
J.Kretowska@kmb.pb.bialystok.pl
Czeslaw MIEDZIALOWSKI. Professor, Chair of Structural Mechanics,
Institute of Civil Engineering at the Bialystok Technical University
(Poland), Dr Habil. Member of Computer Methods Association, Polish
Society of Theoretical and Applied Mechanics, Polish Civil Engineers and
Technicians Association. His research interests include problems of
soil-structure interaction and computer analysis of building structures.
Tadeusz CHYZY. Associate Professor, the Chair of Structural
Mechanics, Institute of Civil Engineering at the Bialystok Technical
University (Poland), where he received his PhD degree. Member of
Scientific Committee of Polish Civil Engineers and Technicians
Association. His research interests include the structures behaviour
under seismic and paraseismic impacts, problems of gas explosions in the
building structures and utilisation of computer methods for structural
analysis.
Joanna KRETOWSKA. Associate Professor, the Chair of Structural
Mechanics, Institute of Civil Engineering at the Bialystok Technical
University (Poland), where she received her PhD degree. Member of Polish
Civil Engineers and Technicians Association. Her research interests
include problems of soil-structure interaction and computer methods in
structural analysis.
Table 1. Analysis of computational times
Method
Computational time [s]
Division
1 2
MQDES 1 70
1 930
ORCAN 2 3727
4 14889
Table 2. Analysis of computational times
Method
Division Computational time [s]
1 2
MQDES 1 171
1 1750
ORCAN 2 5206