Lourenco 2008
Lourenco 2008
PAULO B. LOURENÇO1
1
Professor
ISISE, University of Minho, Department of Civil Engineering, Portugal
E-mail: pbl@civil.uminho.pt
SUMMARY
The mechanics of masonry structures has been underdeveloped in comparison with other
fields of knowledge, with non-linear analysis being a popular field in research. Here, the
possibilities of using structural component models and detailed models using macro-
modelling and micro-modelling are addressed. The possibility of linking micro- and macro-
approaches through homogenization techniques is highlighted. Finally, recommendations for
material data required for advanced non-linear analysis are provided.
INTRODUCTION
Masonry is usually described as a composite material formed by units and joint, with or
without mortar, and different bond arrangements. It is certain that the problems associated
with modelling ancient and modern masonry structures are very different. Physical evidence
shows us that ancient masonry is a very complex material with three-dimensional internal
arrangement, usually unreinforced, but which can include some form of traditional
reinforcement, see Figure 1. Moreover, these materials are associated with complex structural
systems, where the separation between architectural features and structural elements is not
always clear.
(a) (b)
Figure 1. Examples of different masonry types; (a) irregular stone wall with a complex transverse cross section,
from 18th century in Northern Portugaç; (b) timber braced “Pombalino” system emerging
after the 1755 earthquake in Lisbon
The relevance of the internal structure of masonry in the structural response has been
demonstrated by several authors. Only as an example, Figure 2, shows results in dry stone
shear joints, Lourenço and Ramos (2004). The results indicate that, even for the same
material, the friction and dilatancy angles are very dependent on the roughness of the joint. In
particular, a smooth (polished) surface exhibits very low friction and a rough (artificially
induced by a spike) surface exhibits a negative non-negligible dilatancy angle.
5000 Horizontal force (N)
3750
2500
1250
0
-0.5 -0.4 -0.3 -0.2 -0.1
-1250 0 0.1 0.2 0.3 0.4 0.5
-2500
-3750
-5000
Horizontal displacement (mm)
(a) (b)
Horizontal displacement (mm)
P series 0
1.50
1ºC.
S series -1.5 -1 -0.5 0 0.5 1 1.5
τ = -0.618σ R series -0.05
1.25
r2 = 0.975
Shear stress (N/mm2)
2º C.
Linear (P series)
Linear (S series) -0.1
1.00
τ = -0.561σ
7º C. 6º C. 5º C. 4º C. 3º C.
Linear (R series)
r2 = 0.985 -0.15
0.75
-0.2
0.50
τ = -0.179σ
-0.25
r2 = 0.866 0.25
0.00 -0.3
-2.00 -1.50 -1.00 -0.50 0.00 -0.35
Normal stress (N/mm2) Vertical displacement (mm)
(c) (d)
Figure 2. Behaviour of dry stone masonry joints under shear: (a) test set-up; (b) typical shear response in terms
of horizontal force vs. horizontal displacement; (c) Coulomb envelop for (P)olished, (S)awn and (R)ough stone
surfaces; (d) negative dilatancy (horizontal vs. vertical displacement) for rough stone surfaces
Modern masonry can also exhibit significant variations, not only of materials but also of
building technology, see Figure 3. The choice of materials and the thermal solution,
particularly for the enclosure walls, which is a matter of growing concern, is mostly due to
tradition and local availability of the materials. Also, the use of reinforcement is associated
with tradition and local technological developments, with different approaches from one
country to the other.
The fact that ancient and modern masonry have so much variability in materials and
technology make the task of structural analysis of these structures particularly complex. From
a very simplified perspective, it is possible to distinguish masonry as reinforced and
unreinforced. The presence of (distributed) reinforcement provides masonry with tensile
strength and renders masonry closer to reinforced concrete. In such a case, the orthotropic
behaviour of masonry and the non-linear constitutive behaviour become less relevant, and the
techniques normally used for the design and analysis of reinforced concrete structures can
possibly be used. Conversely, in the case of unreinforced masonry structures, the very low
tensile strength of the material renders the use of non-linear constitutive behaviour more
obvious. This is particularly true in the assessment of existing structures and in seismic
analysis.
(a)
(b)
(c)
Figure 3. Examples of modern masonry: (a) typical European unreinforced masonry used in areas of low
seismicity using thick blocks to comply with thermal and sound regulations;
(b) confined masonry in areas of moderate to high seismicity, again with thick blocks;
(c) different reinforced masonry solutions, adopted in the US, Italy and Switzerland, respectively
Masonry is also usually described as a material exhibiting distinct directional properties due
to the mortar joints, which act as planes of weakness. This description is associated mostly
with the material, whereas a different description can be given at structural level. These
descriptions are briefly reviewed below.
In general, the approach towards the numerical representation of masonry can address the
micro modelling of the individual components, viz. unit (brick, block, etc.) and mortar, or the
macro modelling of masonry as a composite, Rots (1991). Depending on the level of accuracy
and the simplicity desired, it is possible to use the following modelling strategies, see Figure
4: Detailed micro-modelling - units and mortar in the joints are represented by continuum
elements whereas the unit-mortar interface is represented by discontinuum elements;
Simplified micro-modelling - expanded units are represented by continuum elements whereas
the behavior of the mortar joints and unit-mortar interface is lumped in discontinuum
elements; Macro-modelling - units, mortar and unit-mortar interface are smeared out in a
homogeneous continuum. In fact, the term “micro-modelling” is probably not the most
adequate and the term “meso-modelling” would be more reasonable, leaving the former
designation for approaches at a lower scale. But the terms macro and micro-modelling are
now widely accepted by the masonry community.
The simplest approach related to the modelling of masonry buildings is given by the
application of different structural elements resorting to e.g. truss, beam, panel, plate or shell
elements to represent columns, piers, arches and vaults, with the assumption of homogeneous
(macro) material behaviour. Figure 5 illustrates various possibilities. The lumped approach or
mass-spring-dashpot model of Figure 5a is at best a crude approximation of the actual
geometry of the structure, using floor levels and lumped parameters as structural components.
The simplicity of the geometric model allows increased complexity on the loading side and in
the non-linear dynamic response. The structural component model in Figure 5b approximates
the actual structural geometry more accurately by using beams and joints as structural
components. This approach allows the assessment of the system behaviour in more detail. In
particular, it is possible to determine the sequential formation of local, predefined failure
mechanisms and overall collapse, both statically and dynamically. Finally, the structural
model in Figure 5c approximates the actual structural geometry using macro-blocks with a
discrete set of failure lines. Most of these efforts address seismic design and assessment, see
Magenes (2006) for details.
The finite element model seems to be the most adequate tool for the application of continuum
macro-models in which structural elements are represented in detail and local failure can be
clearly captured. Figure 6 shows the results of modelling a shear wall with an initial vertical
pre-compression pressure, a wall panel subjected to out of plane failure and a full structure of
a church subjected to foundation settlements. In recent years some effort has been made to
implement finite element limit analysis, Sutcliffe et al. (2001) and Milani et al. (2006a,b,c).
Difficulties of conceiving and implementing macro-models for the analysis of masonry
structures arise especially due to the intrinsic complexity of formulating anisotropic inelastic
behaviour. Only a reduced number of authors tried to develop specific models for the analysis
of masonry structures, e.g. Dhanasekar et al. (1985), Lourenço et al. (1998), Berto et al.
(2002), using different inelastic criteria for tension and compression, typically including
anisotropic material behaviour and different hardening/softening behaviour along each
material axis.
Mass M2
Mass M1
The typical characteristics of discrete element methods are: (a) the consideration of rigid or
deformable blocks (in combination with FEM); (b) connection between vertices and sides /
faces; (c) interpenetration is usually possible; (d) integration of the equations of motion for
the blocks (explicit solution) using the real damping coefficient (dynamic solution) or
artificially large (static solution). The main advantages are an adequate formulation for large
displacements, including contact update, and an independent mesh for each block, in case of
deformable blocks. The main disadvantages are the need of a large number of contact points
required for accurate representation of interface stresses and a rather time consuming analysis,
especially for 3D problems. Discrete elements have been used for masonry e.g. in Azevedo et
al. (2000).
(a) (b) (c)
Figure 7. Examples of cracking at failure using structural micro-modelling: (a) shear wall with opening; (b) wall
subjected to out-of-plane loading; (c) retaining wall.
The finite element method remains the most used tool for numerical analysis in solid
mechanics and an extension from standard continuum finite elements to represent discrete
joints was developed in the early days of non-linear mechanics, with an early application to
masonry, Page (1978). On the contrary, limit analysis received far less attention from the
technical and scientific community for masonry structures, even with also an early application
in Livesley (1978). Still, limit analysis has the advantage of being a simple tool, while having
the disadvantages that only the collapse load and the collapse mechanism can be obtained and
the loading history can hardly be included. A complete micro-model must include all the
failure mechanisms of masonry, namely, cracking of joints, sliding over one head or bed joint,
cracking of the units and crushing of masonry, Lourenço and Rots (1997). By adopting
appropriate evolution rules in a finite element environment, Oliveira and Lourenço (2004), it
is possible to reproduce non-linear behaviour during unloading. Orduña and Lourenço (2005)
developed a limit analysis constitutive model that incorporates non-associated flow at the
joints, compressive failure and a novel formulation for torsion.
HOMOGENIZATION TECHNIQUES
Homogenisation
The most popular homogenisation approach replaces the complex geometry of the basic cell
by a simplified geometry so that a close-form solution of the homogenisation problem is
possible, e.g. Pande et al. (1989) and Maier et al. (1991). The homogenisation has generally
been performed in two steps, head (or vertical) and bed (or horizontal) joints being introduced
successively. The use of two separate homogenisation steps does not explicitly account for
the regular offset of vertical mortar joints belonging to two consecutive layered unit courses,
which results in significant errors in the case of non-linear analysis. Many other approaches
involving different approximations and ingenious assumptions have been sought, with an
increasing large number of papers in the recent years, e.g. Pietruszczak and Niu (1992), where
a two-stage homogenization procedure was employed with the head joints considered as
uniformly dispersed elastic inclusions and the bed joints assumed to represent a set of
continuous weakness, or Gambarotta and Lagomarsino (1997), Massart et al. (2004), Podestà
(2005), Calderini and Lagomarsino (2006), where simplified non-linear homogenisation
techniques were used.
When the basic cell is loaded only with normal stresses, the micromechanical model of
Zucchini and Lourenço (2002) assumes that all shear stresses and strains inside the basic cell
can be neglected, except the in-plane shear stress and strain (σxy and εxy) in the bed joint and
in the unit. The non-zero stresses and strains in the bed joint, head joint and unit are assumed
to be constant, with the exception of the normal stress σxx in the unit, which is a linear
function of x and accounts for the effect of the shear σxy in the bed joint, and with the
exception of the shear stress σxy in the unit, which is linear in y. The coupling of this model
with non-linear constitutive models, leads to an iterative algorithm, in which at each cycle a
system of equilibrium equations is solved to obtain the unknown effective stresses and strains.
The model was applied to a real masonry basic cell and compared with the results of an
accurate finite element analysis (FEA) under linear elastic analysis. In the finite element
analysis and the analytical model, the properties of the components can be taken absolutely
equal. Different stiffness ratios between mortar and unit are considered. The material
properties of the unit are kept constant, whereas the properties of the mortar are varied to
yield a ratio Eb / Em ranging from 1 to 1000. The adopted range is very large, if only linear
elastic behaviour of mortar is considered. However, those high values are indeed encountered
if inelastic behaviour is included. In such case, Eb and Em should be understood as linearised
tangent Young’s moduli, representing a measure of the degradation of the (tangent / secant)
stiffness matrices utilised in the numerical procedures adopted to solve the non-linear
problem. Note that the ratio Eb / Em tends to infinity when softening of the mortar is complete
and only the unit remains structurally active. The elastic properties of the homogenised
material, calculated by means of the proposed micro-mechanical model, are compared in
Figure 10a with the values obtained by FE analysis. The agreement is very good in the entire
range 1≤ Eb / Em ≤1000, with a maximum error ≤ 6%. A comparison between the results
obtained with the micro-mechanical model and the experimental results of Page (1981,1983)
are given in Figure 10b. Very good agreement is found in the shape of the yield surface,
indicating that the proposed model can be used as a possible macro-model to represent the
composite failure of masonry.
Figure 11 shows the validation of the model under non-linear uniaxial loading. The algorithm
has been tested in the fracture problem of an infinitely long wall under tensile loading parallel
to the bed joint (Figure 11a), which has been analysed by Lourenco et al. (1999) with a
sophisticated finite element interface model based on multisurface plasticity. The model
reproduces with good agreement the FE analysis of the cell degradation and the two peaks of
the failure load for a zero dilatancy angle in the joints. The head joint is the first to fail in
tension and the bed joint takes its place in the load carrying mechanism of the cell. The load is
transferred through bed joint shear from unit to the other, with the cell showing regained
elastic behaviour for increasing loads, until final failure of the bed joint in shear. The residual
load carrying capacity is zero because there is no vertical compression, and therefore no
friction effect.
(a) (b)
Figure 10. Elastic results for the micro-mechanical model: (a) comparison of Young’s moduli with FEA results
for different stiffness ratios; (b) comparison with experimental results of Page (1981,1983).
(a) (b)
Figure 11. Inelastic response of the model: (a) post-peak tensile behaviour and comparison with FEM results of
Lourenco et al. (1999); (b) axial stress vs. axial strain and comparison between finite element
simulation of Lourenço and Pina-Henriques (2006).
Figure 11b shows the behaviour of a basic masonry cell under axial compressive loading
perpendicular to the bed joint and a comparison with an accurate FE calculation of Lourenço
and Pina-Henriques (2006). The curves obtained with the homogenisation model almost
coincide with the corresponding FE results, with marginal computational effort and no
convergence difficulties. For weak mortars the plastic flow of the mortar joints starts very
early in the loading path, while the brick non-linear behaviour begins a little later. The brick
is in a tension-compression-tension state, while the mortar is in a tri-axial compression state
for the lateral containment effect of the stiffer brick. The head joint suffers some negligible
damage in tension just before the complete failure of the brick in tension, which leads to the
catastrophic failure of the entire cell. For strong mortars the plastic flow starts earlier in the
brick than in the bed joint, due to the higher strength of the mortar. The inversion of the
elastic mismatch between mortar and brick in this case (the mortar is much stiffer than the
brick) yields in this case a tension-tension-compression state of the bed joint. A substantial
(57%) isotropic damage in tension is reached in the bed joint, but the failure of the masonry
cell is driven again by the crushing of the brick. The damage of the mortar in the bed is due to
the high tension in the x and z direction.
A stress field expansion approach
Using the lower bound theorem of limit analysis and the hypotheses of homogenization, a
solution for the homogenization problem can be derived by means of a (non-linear)
optimization problem. Here, the masonry cell is sub-divided into thirty-six sub-domains,
Milani et al. (2006a). For each sub-domain, polynomial distributions of cubic degree are
assumed for the stress components. Details on equilibrium and anti-periodicity conditions,
and validation of the approach are shown in Milani et al. (2006a,b). Extension of the
formulation to out-of-plane behaviour is given in Milani et al. (2006c).
The clay masonry shear walls tested by Ganz and Thürlimann (1984) at ETH Zurich and
analysed in Lourenço (1996) are shown here for validation. In Figure 12a,b the principal
stress distribution at collapse from the lower bound analysis and the velocities at collapse
from the upper bound analysis are reported. Good agreement is found among the model here
proposed, the incremental elastic-plastic analysis reported in Lourenço (1996) and
experimental data. Finally, in Figure 12c a comparison between the numerical failure loads
provided respectively by the lower and upper bound approaches and the experimental load-
displacement diagram is reported. Collapse loads P(–) = 210 kN and P(+) = 245kN are
numerically found using a model with 288 triangular elements, whereas the experimental fail-
ure shear load is approximately P = 250 kN.
2500
2000
2000
1500
y [mm] 1500
1000 y [mm]
1000
500
500
0 0
300
250
Horizontal Load [kN]
200
Experimental
150 Limit Analysis
100
50
Milani et al. (2006c) further extended and validated the formulation of the previous section to
out-of-plane loading, where the elementary cell is subdivided along the thickness in several
layers. The homogenized model is also employed in order to reproduce experimental data for
panels out-of-plane loaded. Figure 13a shows typical comparisons between experimental
pressure-displacement curves by Chong et al. (1995), numerical pressure-displacement curves
obtained by means of an orthotropic elasto-plastic macro-model (Lourenço, 2000) and the
results with the proposed formulation. Figure 13b shows results of the numerical analysis in
terms of ultimate principal moment distribution and failure mechanisms. The agreement with
experimental results is worth noting in all cases analysed. Finally, some real scale application
of the model to a building in Italy is shown in Figure 13c, demonstrating the possibility of
using the proposed tools for safety evaluation. In this case, a complex collapse mechanism
involving piers and walls has been found.
2.5
2.34 U.B.
2.25 L.B.
2.0
p [kN/m2 ]
1.5
0.5
Panel SB02
2500
0.0 5.0 10.0 15.0 20.0 25.0
2000
Max displacement [mm] 1500
1000
0 500
1000 2000 3000 4000 5000 0
6000
(a) (b)
(c)
Figure 13. Results involving out-of-plane loading: (a) comparison between experimental and numerical results
for masonry wall subjected to out-of-plane loading; (b) lower (principal moments at collapse)
and upper bound results (deformed mesh at collapse and yield line pattern) for the same
wall; (c) collapse of a masonry building subjected to earthquake action.
Extensive information on the tensile strength and fracture energy of units exists, see van der
Pluijm (1999), Lourenço et al. (2005), Vasconcelos et al. (2007). The ductility index du, given
by the ratio between the fracture energy Gf and the tensile strength ft, found for brick was
between 0.018 and 0.040 mm, as shown in Table 1 and Table 2. It is normal that the values
are different because different testing procedures and different techniques to calculate the
fracture energy have been used. Therefore, the recommended ductility index du, in the
absence of more information is the average, 0.029 mm.
Table 2. Ductility index for different bricks, van der Pluijm (1999)
ft// / ft⊥ ft// du
Bricks
[-] [N/mm2] [mm]
VE 1.64 2.47 0.0367
JC 1.49 3.51 0.0430
Average 1.6 3.0 0.040
For stone granites, it is noted that a non-linear relation, Vasconcelos et al. (2007) given by
du = 0.239 ft – 1.138 was found, with du in mm and ft in N/mm2. For an average granite tensile
strength value of 3.5 N/mm2, the du value reads 0.057 mm, which is the double of the
suggested value for brick. Model Code 90, CEB-FIP (1993), recommends for concrete
(maximum aggregate size 8 mm), the value of Gf = 0.025 (fc / 10)0.7, with Gf in N/mm and the
compressive strength fc in N/mm2. Assuming that the relation between tensile and
compressive strength is 5%, Lourenço et al. (2004), the following expression is obtained Gf =
0.025 (2 ft)0.7. For an average tensile strength value of 3.5 N/mm2, Gf is equal to 0.0976
N/mm and du reads 0.028 mm, which is similar to the suggested value for brick. For the
mortar, standard test specimens are cast in steel moulds and the water absorption effect of the
unit is ignored, being thus non-representative of the mortar inside the composite. For the
tensile fracture energy of mortar, and due to the lack of experimental results, it is
recommended to use values similar to brick, as indicated above.
The research on masonry has been scarce when compared with other structural materials and
experimental data which can be used as input for advanced non-linear models is limited. The
parameters needed for the tensile mode (Mode I) are similar to the previous section, namely
the bond tensile strength ft and the bond fracture energy Gf. The factors that affect the bond
between unit and mortar are highly dependent on the units (material, strength, perforation,
size, air dried or pre-wetted, etc.), on the mortar (composition, water contents, etc.) and on
workmanship (proper filling of the joints, vertical loading, etc.). A recommendation for the
value of the bond tensile strength based on the unit type or mortar type is impossible, but an
indication is given in Eurocode 6, CEN (2005). It is stressed that the tensile bond strength is
very low, Rots (1997) and van der Pluijm (1999), typically in the range of 0.1 to 0.2 N/mm2.
Limited information on the non-linear shear behavior of the interface (Mode II) also exists,
Rots (1997) and van der Pluijm (1999). A recommendation for the value of the bond shear
strength (or cohesion) based on the unit type or mortar type is impossible, but an indication is
again given in Eurocode 6, CEN (2005). The ductility index du, s, given by the ratio between
the fracture energy Gfs and the cohesion c, found for different combinations of unit and mortar
was between 0.062 mm and 0.147, as shown in Table 3. The recommended ductility index
du, s, in the absence of more information, is the average value of 0.093 mm. It is noted that the
Mode II fracture energy is clearly dependent of the normal stress level, van der Pluijm (1999),
and the given values hold for a zero normal stress.
The parameters needed for characterizing the non-linear compressive behavior are the peak
strain and the post-peak fracture energy. The values proposed for concrete in the Model Code
90, CEB-FIP (1993) are a peak strain of 0.2 % and a total compressive fracture energy Gfc
given by the best fit Gfc = 15 + 0.43 fc – 0.0036 fc2 , with Gfc in N/mm and the compressive
strength fc in N/mm2. This curve is only applicable for fc values between 12 and 80 N/mm2.
The average ductility index in compression du,c resulting from the average value of the best fit
is 0.68 mm, even if this value changes significantly. Therefore, for compressive strength
values between 12 and 80 N/mm2, the expression for the compressive fracture energy above is
recommended. For fc values lower than 12 N/mm2, a du,c value equal to 1.6 mm is suggested
and for fc values higher than 80 N/mm2, a du,c value equal to 0.33 mm is suggested. These are
the limits obtained from Model Code 90.
CONCLUSIONS
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reinforced and unreinforced masonry structures, European Committee for Standardization,
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out-of-plane loaded masonry walls”, Journal of Structural Engineering, ASCE, 2006c,
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the cyclic behavior of interface elements”, Computers & Structures, 82 (17-19), 2004, pp
1451-1461.
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