This paper focuses on the numerical simulation of the deformation processes occurring in the slopes when soils with strain-softening behaviour are involved. In these circumstances, a progressive failure may occur with the consequent motion of the unstable soil mass in the post-failure stage. This problem can be only solved using advanced numerical techniques capable also of accounting for the occurrence of large deformations. However, the solution is generally mesh dependent and may be affected by lack of convergence. In this study, the material point method is employed to simulate the occurrence of large deformations, in conjunction with a strain-softening Mohr–Coulomb constitutive model, in which the shear strength parameters are reduced as a function of the accumulated deviatoric plastic strain, and a model parameter controlling the rate of strength decrease. To evaluate this parameter and to reduce the effects of the mesh dependency on the numerical solution, a novel procedure based on the results of direct shear tests is presented. This methodology is completely analytical and requires few parameters with a clear physical meaning and of simple experimental determination. Some simulations are performed to assess the reliability of the proposed procedure.

Deformation processes of the slopes are usually categorised into four distinct phases (Leroueil, 2001): pre-failure, failure, post-failure and eventual reactivation. Soil brittleness undoubtedly affects the pre-failure phase due to the occurrence of a progressive failure (Bishop, 1967), but it could also play an important role in the kinematics of the unstable soil mass during the post-failure phase (Leroueil, 2001). Deformation and failure mechanisms of the slopes can be effectively analysed using numerical methods capable of simulating both the progressive development of shear zones within the slope and the run-out process of the landslide. In this paper, the material point method (MPM) is used for analysing the deformation processes that occur in slopes consisting of soils with strain-softening behaviour (Yerro et al., 2016; Fern et al., 2019; Conte et al., 2020; Alonso, 2021). In these circumstances, the solution is often affected by a lack of convergence and a strong dependency on the employed mesh (Soga et al., 2016). This problem can be overcome using the so-called regularisation techniques. However, these techniques are generally very expensive from a computational viewpoint. A simple-to-use procedure based on the results of conventional direct shear tests, is proposed herein to reduce the numerical problems due to mesh dependency. This methodology is completely analytical and requires few parameters with a clear physical meaning. A case study is analysed to show the effectiveness of the proposed approach.

An original procedure is presented to reduce the mesh dependency when dealing with brittle soils. This procedure utilises, in the context of a strain-softening Mohr–Coulomb model, a strength reduction law similar to that proposed by Yerro et al. (2016) in which the cohesion intercept c′ and the angle of shearing resistance φ′ of the soil reduce with an increase of the deviatoric plastic strain invariant εdp, according to the following equations:

1
2

where

3

eijp is the deviatoric part of the plastic strain tensor, and the model parameter λ controls the strength reduction rate. The proposed procedure is analytical and is based on the results of direct shear tests. Specifically, a complete sequence of shearing cycles necessary to attain the residual strength of the involved soil is required. Figure 1 shows an example of these data. In this figure, δp is the horizontal displacement when peak strength occurs, δpp is the horizontal displacement (net of δp) corresponding to the post-peak condition (in the first shearing cycle) and δr is the net horizontal displacement at which the shear strength attains the residual condition. Moreover, τp, τpp and τr are the peak, post-peak and residual shear strength of the soil, respectively (Calabresi & Manfredini, 1973).

In the proposed method, the following equation is assumed to relate the soil shear strength to the plastic shear strain γp:

4
Fig. 1.

Shearing cycles of a direct shear test with the τδ relationship provided by equation (5)

Fig. 1.

Shearing cycles of a direct shear test with the τδ relationship provided by equation (5)

Close modal

The plastic shear strain is expressed as γp=δδp/l, where l is the thickness of the shear zone and δ is the total horizontal displacement. As a consequence, equation (4) takes the form:

5

with δ>δp.

Considering the first shearing cycle (Fig. 1), the ratio λ/l can be calculated by replacing τ=τpp and δδp=δpp into equation (5). The resulting expression for λ/l is

6

where the values of τp, τpp, τr and δpp are evaluated from the τδ curve obtained experimentally (Fig. 1). It is worth noting that equation (6) provides directly the ratio λ/l rather than the parameters λ and l, which are difficult to be evaluated separately. Once λ/l is calculated using equation (6), it needs to check whether equation (5) approaches the residual value τr when δδp=δr. To this end, the ratio β may be considered:

7

in which τr denotes the shear strength calculated using equation (5) with δδp=δr. The resulting value of β should be close to zero to ensure a good agreement between experimental and analytical curves. Otherwise, new values of τpp and δpp are assumed and the above-described steps are again performed until β results close to zero. Referring to the experimental data shown in Fig. 1, a ratio λ/l = 300 m−1 is evaluated using this iterative procedure. The τδ relationship provided by equation (5) along with this value of λ/l is plotted in blue in the same figure. The resulting relationship approximates the experimental data very well.

It is worth noting that the thickness l of the shear zone in a direct shear test is related to the soil grain size, whereas in the numerical simulations this thickness depends on the mesh size, L (Fig. 2). Likewise, the model parameter λ from the direct shear tests may be different from that adopted in the calculations. This latter is herein denoted λ* to distinguish it from the former. An evaluation of λ* is performed in this study by imposing the same τδ relationship (from peak to residual) obtained from the direct shear tests, to the soil of the shear zone in the numerical simulation (Fig. 2). Under this assumption, equation (5) takes the form:

8
Fig. 2.

Scheme showing a shear zone in a direct shear test with thickness l and ratio λ/l, and that in a numerical simulation with thickness L and ratio λ*/L

Fig. 2.

Scheme showing a shear zone in a direct shear test with thickness l and ratio λ/l, and that in a numerical simulation with thickness L and ratio λ*/L

Close modal

Consequently, equation (6) expresses both λ/l for the direct shear test, and λ*/L for the numerical simulation. To support this assumption, some numerical analyses concerning an ideal shear test under plane strain conditions are performed using the finite-element code, Tochnog Professional (Roddeman, 2022). It is assumed that the tested soil sample consists of a material characterised by the experimental τδ relationship shown in Fig. 1 with λ/l = 300 m−1. The shear zone has a thickness equal to L. Meshes with a different size are employed to discretise this shear zone. Specifically, the following values of L are considered: 1, 10, 50 and 100 cm. A comparison between experimental and predicted τδ relationships (from peak to residual) is presented in Fig. 3 for different values of λ* and L, but with the same ratio λ*/L = 300 m−1 coincident with λ/l deduced experimentally (Fig. 1). A very close agreement between simulation results and experimental data is obtained under these conditions (λ*/L = λ/l, for a given L). In other words, the model parameter λ* depends on the mesh size L and is related to the ratio λ/l deduced from the direct shear tests.

Fig. 3.

Comparison between the experimental results of a direct shear test and the τδ relationship predicted by FEM using different values of λ* and L, but with the same ratio λ*/L

Fig. 3.

Comparison between the experimental results of a direct shear test and the τδ relationship predicted by FEM using different values of λ* and L, but with the same ratio λ*/L

Close modal

Summarising, the following simple procedure is proposed to reduce the influence of the mesh dependency on the slope response when soils with strain-softening behaviour are involved. Ratio λ/l is first evaluated from the available data of direct shear tests using equation (6) along with the iterative procedure previously described. Once this ratio is known, the model parameter λ* to be used in the numerical simulation in which a mesh with a given size L is employed, can be evaluated as follows:

9

This approach was recently used in conjunction with MPM to simulate successfully the deformation processes of a landslide in brittle soils (Troncone et al., 2022).

To assess the capability of the proposed procedure to reduce the mesh-dependency influence on the numerical results, an ideal slope constituted by a brittle soil with different strength reduction rates is considered. This slope is characterised by a height of 15 m and an inclination angle of 45° (Fig. 4), and consists of a homogeneous dry soil whose properties are indicated in Table 1, in which γ is the unit weight, E′ is the Young modulus, ν′ is the Poisson ratio and ψ is the dilatancy angle. Figure 5 shows three τδ curves obtained from direct shear tests. These curves have the same peak strength and the same residual strength, but a different strength reduction rate with values of λ/l equal to 100, 300 and 600 m−1, respectively. As shown in Fig. 5, the higher the value of λ/l, the faster the strength reduction from peak to residual. To trigger a deformation process in the slope, an excavation 5 m deep is carried out at the slope toe, as indicated in Fig. 4. For the sake of completeness, the safety factor of the slope is first evaluated using the limit equilibrium method (Morgenstern & Price, 1965). The resulting values are 3·73 and 0·75 when the peak shear strength parameters and the residual ones are used in the calculations, respectively. As a consequence, a progressive failure may occur due to the excavation (Bjerrum, 1967). The deformation processes occurring in the slope (from the pre-failure phase to the post-failure one) are simulated using the MPM code Anura3D (www.anura3d.com). In this context, different meshes with L = 0·5, 1 and 1·5 m are considered. Each mesh is made up of triangular elements and any active element contains initially three material points. Both vertical and horizontal displacements are constrained at the bottom of the domain and the horizontal displacements are prevented on the vertical sides. The initial stress state of the slope is reproduced using the well-known gravity loading procedure. Afterwards, the excavation is simulated by removing the material points located in the area indicated in Fig. 4. The values of the model parameter λ* to be used in the simulation are evaluated as a function of λ/l and L using the procedure described in the previous section. The resulting values of λ* are listed in Table 2.

Fig. 4.

Slope model considered in the analysis with indication of the excavation zone

Fig. 4.

Slope model considered in the analysis with indication of the excavation zone

Close modal
Fig. 5.

τδ curves assumed in the analysis with indication of the associated value of λ/l

Fig. 5.

τδ curves assumed in the analysis with indication of the associated value of λ/l

Close modal
Table 1.

Soil parameters used in the analyses

γ: kN/m3E′: kPaν′: dimensionlesscp: kPaφp: °cr: kPaφr: °ψ: °
1630 0000·3120308230
Table 2.

Values of the parameter λ* used in the numerical simulations

λ/l: m−1λ* (L = 0·5 m)λ* (L = 1·0 m)λ* (L = 1·5 m)
10050100150
300150300450
600300600900

Some simulation results are documented in Figs. 6–8, where for each value of λ/l a comparison in terms of the final displacement field calculated using a different mesh size is presented. These results show that the slope response depends on the value of λ/l expressing the strength reduction rate in the direct shear test. Specifically, when λ/l = 100 m−1, the soil strength reduction is slow and the slope only undergoes small displacements (Fig. 6). In other words, the excavation performed at the slope toe is not sufficient to reduce the soil strength to the point of causing a slope failure. On the contrary, the slope collapses when the higher values of λ/L are assumed – that is, 300 m−1 (Fig. 7) and 600 m−1 (Fig. 8). In these circumstances, a rapid reduction of the soil strength occurs due to the excavation up to causing a slope failure. This result is found for all employed meshes that are characterised by the same ratio λ*/L assumed equal to the associated λ/l, according to the proposed procedure. In Figs. 7 and 8, the run-out distance (defined as the distance between the tip of the displaced material and the vertical wall of the excavation) is also indicated. As can be observed from the presented results, the final configuration of the displaced material, the displacement magnitude and the run-out distance are slightly affected by the mesh size, provided that the same value of λ*/L (with λ*/L= λ/l) is employed in the simulation. The greatest discrepancy found in terms of soil displacement for the different values of λ*/L considered, is about 10%. In addition, the values of the run-out distance differ from each other of a few decimetres. It is also worthy to note that in Figs. 6(c) and 7(a) the value of λ* = 150 is used with a different mesh size (L = 1·5 m and L = 0·5 m, respectively) and consequently with a different value of λ*/L (100 and 300 m−1, respectively). As can be seen by comparing Figs. 6(c) and 7(a), very different results are obtained when λ* and L are arbitrarily chosen without accounting for the ratio λ/l obtained experimentally. Summarising, shape factor λ* is mesh dependent, but this dependency can be reduced by assuming a constant value of λ*/L that is equal to λ/l obtained from the τδ relationship of a direct shear test using the procedure proposed in the present study. This assertion is also corroborated by the results shown in Figs. 9(a)–9(c), which document the time–total displacement relationship at point P, whose initial location is indicated in Fig. 4, for the different mesh sizes and the different values of λ*/L considered.

Fig. 6.

Final total displacement field for different meshes characterised by the same ratio λ*/L = 100 m−1: (a) λ* = 50 and L = 0·5 m; (b) λ* = 100 and L = 1 m; (c) λ* = 150 and L = 1·5 m

Fig. 6.

Final total displacement field for different meshes characterised by the same ratio λ*/L = 100 m−1: (a) λ* = 50 and L = 0·5 m; (b) λ* = 100 and L = 1 m; (c) λ* = 150 and L = 1·5 m

Close modal
Fig. 7.

Final total displacement field for different meshes characterised by the same ratio λ*/L = 300 m−1: (a) λ* = 150 and L = 0·5 m; (b) λ* = 300 and L = 1 m; (c) λ* = 450 and L = 1·5 m

Fig. 7.

Final total displacement field for different meshes characterised by the same ratio λ*/L = 300 m−1: (a) λ* = 150 and L = 0·5 m; (b) λ* = 300 and L = 1 m; (c) λ* = 450 and L = 1·5 m

Close modal
Fig. 8.

Final total displacement field for different meshes characterised by the same ratio λ*/L = 600 m−1: (a) λ* = 300 and L = 0·5 m; (b) λ* = 600 and L = 1 m; (c) λ* = 900 and L = 1·5 m

Fig. 8.

Final total displacement field for different meshes characterised by the same ratio λ*/L = 600 m−1: (a) λ* = 300 and L = 0·5 m; (b) λ* = 600 and L = 1 m; (c) λ* = 900 and L = 1·5 m

Close modal
Fig. 9.

Time evolution of the total displacement of the material point P located in Fig. 4, for different mesh sizes and with (a) λ*/L = 100 m−1; (b) λ*/L = 300 m−1; (c) λ*/L = 600 m−1

Fig. 9.

Time evolution of the total displacement of the material point P located in Fig. 4, for different mesh sizes and with (a) λ*/L = 100 m−1; (b) λ*/L = 300 m−1; (c) λ*/L = 600 m−1

Close modal

Finally, Figs. 10–12 show the calculated deviatoric strain distribution. Consistently with the results in terms of displacements (Figs. 6–8), the induced deformations are low when λ/l = 100 m−1 (Fig. 10), whereas a slope failure occurs when the higher values of λ/l are assumed (Figs. 11 and 12). In these latter circumstances, the shape and location of the failure surface are very similar when the same value of λ*/L is adopted in the analysis. Although the strain magnitude is different, it is important that the product λεdp is mesh-independent because it appears in equations (1) and (2) defining the softening law of the soil. In this connection, Figs. 13(a)–13(c) show the time evolution of λεdp calculated in the material point Q for the considered values of λ* and L. Point Q is located in Fig. 4 and falls within the shear zone, where large deviatoric strains occur when λ*/L = 300  and 600 m−1. As can be seen,  λεdp is essentially unaffected by the mesh size, confirming the effectiveness of the proposed method.

Fig. 10.

Final deviatoric strain field for different meshes characterised by the same ratio λ*/L = 100 m−1: (a) λ* = 50 and L = 0·5 m; (b) λ* = 100 and L = 1 m; (c) λ* = 150 and L = 1·5 m

Fig. 10.

Final deviatoric strain field for different meshes characterised by the same ratio λ*/L = 100 m−1: (a) λ* = 50 and L = 0·5 m; (b) λ* = 100 and L = 1 m; (c) λ* = 150 and L = 1·5 m

Close modal
Fig. 11.

Final deviatoric strain field for different meshes characterised by the same ratio λ*/L = 300 m−1: (a) λ* = 150 and L = 0·5 m; (b) λ* = 300 and L = 1 m; (c) λ* = 450 and L = 1·5 m

Fig. 11.

Final deviatoric strain field for different meshes characterised by the same ratio λ*/L = 300 m−1: (a) λ* = 150 and L = 0·5 m; (b) λ* = 300 and L = 1 m; (c) λ* = 450 and L = 1·5 m

Close modal
Fig. 12.

Final deviatoric strain field for different meshes characterised by the same ratio λ*/L = 600 m−1: (a) λ* = 300 and L = 0·5 m; (b) λ* = 600 and L = 1 m; (c) λ* = 900 and L = 1·5 m

Fig. 12.

Final deviatoric strain field for different meshes characterised by the same ratio λ*/L = 600 m−1: (a) λ* = 300 and L = 0·5 m; (b) λ* = 600 and L = 1 m; (c) λ* = 900 and L = 1·5 m

Close modal
Fig. 13.

Time evolution of λ*εdp calculated in the material point Q located in Fig. 4, for: (a) λ*/L = 100 m−1; (b) λ*/L = 300 m−1; (c) λ*/L =  600 m−1

Fig. 13.

Time evolution of λ*εdp calculated in the material point Q located in Fig. 4, for: (a) λ*/L = 100 m−1; (b) λ*/L = 300 m−1; (c) λ*/L =  600 m−1

Close modal

The proposed procedure appears quite attractive for practical purposes because it is simple to use and requires few parameters as input data. However, some aspects concerning its application to real case studies should be clarified. Although the present method is herein used in conjunction with MPM, it could also be employed with different mesh-dependent numerical techniques in which the softening rule considered in the present study is implemented. In addition, the proposed method is based on the results of the direct shear test that is simple and very widespread in engineering applications. However, it is often criticised for the non-uniformity of stress and strain applied to the sample due to the boundary conditions imposed by the box. Potts et al. (1987) analysed in detail this aspect and showed that the above-mentioned non-uniformity slightly affects the load–displacement behaviour of the soil. Finally, considering that the model parameter λ* depends on L, a uniform mesh should be used for homogeneous soils. However, this could be very expensive from a computational viewpoint, especially when the slope is particularly long. To overcome this issue, the layers of homogenous soil may be split into some smaller regions (clusters) with a different size L but with the same value of λ*/L.

A novel methodology has been proposed to reduce the numerical problems due to mesh dependency, which arise when soils with strain-softening behaviour are involved in the deformation processes of slopes. The method is completely analytical and simple to use. It is based on the experimental data from direct shear tests inclusive of the shearing cycles necessary to reduce the soil strength from peak to residual. In addition, a negative exponential law is employed to match the experimental τδ curves provided by these tests, and an iterative and quickly converging procedure is developed to evaluate the ratio of the model parameter λ controlling the strength reduction rate, to the thickness of the shear zone in the direct shear tests, l. Once λ/l is known, the model parameter λ* to be used in the numerical simulation can be determined for a given mesh size L, using a simple equation (equation (9)). The numerical simulations performed in the present study using MPM corroborate the reliability of the proposed method.

All data used are available from the corresponding author by request.

c

cohesion intercept

cp

peak value of cohesion intercept

cr

residual value of cohesion intercept

E

Young's modulus

eijp

deviatoric part of the plastic strain tensor

L

thickness of the shear zone in numerical simulation

l

thickness of the shear zone in direct shear test

β

ratio defined by equation (7)

γ

unit weight

γp

plastic shear strain in the shear zone

δ

horizontal displacement in direct shear test

δp

horizontal displacement corresponding to the peak strength in direct shear test

δpp

horizontal displacement (net of δp) corresponding to the post-peak condition in direct shear test

δr

horizontal displacement (net of δp) corresponding to the residual condition in direct shear test

εdp

deviatoric plastic strain invariant

λ

model parameter controlling the strength reduction rate in direct shear test

λ

model parameter controlling the strength reduction rate of the shear zone in numerical simulation

ν

Poisson's ratio

τ

shear stress

τp

peak shear strength

τpp

post-peak shear strength

τr

residual shear strength

φ

angle of shearing resistance

φp

peak angle of shearing resistance

φr

residual angle of shearing resistance

ψ

dilatancy angle

Alonso
,
E. E.
(
2021
).
Triggering and motion of landslides
.
Géotechnique
71
, No.
1
,
3
59
, .
Bishop
,
A. W.
(
1967
).
Progressive failure-with special reference to the mechanism causing it
.
Proc. Geotech. Conf.
,
Oslo
. vol.
2
, pp.
142
150
.
Oslo, Norway
:
Norwegian Geotechnical Institute
.
Bjerrum
,
L.
(
1967
).
Progressive failure in slopes of overconsolidated plastic clays and clay shales
.
J. Soil Mech. Found. Engng Div.
93
, No.
5
,
1
49
.
Calabresi
,
G.
&
Manfredini
,
G.
(
1973
).
Shear strength characteristics of the jointed clay of S. Barbara
.
Géotechnique
23
, No.
2
,
233
244
, .
Conte
,
E.
,
Pugliese
,
L.
&
Troncone
,
A.
(
2020
).
Post-failure analysis of the Maierato landslide using the material point method
.
Engng Geol.
277
,
105788
.
Fern
,
J.
,
Rohe
,
A.
,
Soga
,
K.
&
Alonso
,
E.
(
2019
).
The material point method for geotechnical engineering. A practical guide
, (1) st edn.
Boca Raton, FL, USA
:
CRC Press
.
Leroueil
,
S.
(
2001
).
Natural slopes and cuts: movement and failure mechanism
.
Géotechnique
51
, No.
3
,
197
243
.
Morgenstern
,
N. R.
&
Price
,
V. E.
(
1965
).
The analysis of the stability of general slip surfaces
.
Géotechnique
15
, No.
1
,
79
93
, .
Potts
,
D. M.
,
Dounias
,
G. T.
&
Vaughan
,
P. R.
(
1987
).
Géotechnique
37
, No.
1
,
11
23
, .
Roddeman
,
D. G.
(
2022
).
Tochnog professional
.
User's manual Tochnog Professional Company
.
Soga
,
K.
,
Alonso
,
E.
,
Yerro
,
A.
,
Kumar
,
K.
&
Bandara
,
S.
(
2016
).
Trends in large-deformation analysis of landslide mass movements with particular emphasis on the material point method
.
Géotechnique
66
, No.
3
,
248
273
, .
Troncone
,
A.
,
Pugliese
,
L.
&
Conte
,
E.
(
2022
).
Analysis of an excavation-induced landslide in stiff clay using the material point method
.
Engng Geol.
296
,
106479
.
Yerro
,
A.
,
Alonso
,
E. E.
&
Pinyol
,
N. M.
(
2016
).
Run-out of landslides in brittle soils
.
Comput. Geotech.
80
,
427
439
.
This is an open-access article distributed under the terms of the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

or Create an Account

Close Modal
Close Modal