Abstract
A method based on the application of KΓΆtterβs equation is proposed for the complete analysis of active thrust on an inclined wall with inclined cohesionless backfill under surcharge effect. Coulombβs failure mechanism is considered in the analysis. The point of application of active thrust is determined from the condition of moment equilibrium. The coefficient of active pressure and the point of application of the active thrust are computed and presented in nondimensional form. One distinguishing feature of the proposed method is its ability to determine the point of application of active thrust on the retaining wall. A fairly good comparison is obtained with the existing solutions.
1. Introduction
Active earth pressure evaluation is required for the design of geotechnical structures such as retaining walls, sheet piles, basements, and tunnels. Active thrust acting on a retaining wall is dependent of many parameters. The theories proposed by Coulomb [1] and Rankine [2] remain the fundamental approaches to analyze the active earth pressures. Coulomb [1] studied the earth pressure problems using the limit equilibrium method considering a triangular wedge of backfill behind a rough retaining wall with a plane failure surface and this theory is well verified for the frictional soil in active state. The point of application of active thrust is assumed at a distance one-third of the height of the wall from its base and independent of different parameters such as soil friction angle, , angle of wall friction, , backfill angle, , and wall inclination angle. Coulombβs [1] approach does not use moment equilibrium equation for the analysis, since the distribution and point of application of reaction on the failure plane are unknown. If the distribution and point of application of soil reaction on the failure plane are known, then the point of application of active thrust can be determined using moment equilibrium equation. The limit equilibrium method assuming appropriate failure surface is most frequently used to analyze static earth pressure.
A failure mechanism was proposed by Terzaghi [3] that assumes a log-spiral failure surface originating from the base of the wall, followed by a tangent, that meets the ground surface at an angle corresponding to Rankineβs [2] active earth pressure. Several experimental, analytical, and numerical studies were performed to evaluate the earth pressures on the retaining walls [4β14]. Some rigorous approaches such as finite element methods were attempted to determine the distribution of earth pressures on the retaining wall. Others prepared the tables for the calculation earth pressures based on log-spiral failure surface [15]. Active earth pressure coefficients for cohesionless soil were also computed using the method of slices by considering the soil mass in the state of limit equilibrium [16, 17]. The charts were prepared for the calculation earth pressures based on log-spiral failure surface [18]. Discrete element analysis is used to evaluate active and passive pressure distributions on the retaining wall [19].
Recently the active earth pressure coefficients were computed based on the lower bound theorem of plasticity [20]. Upper-bound theorem of limit analysis was used to evaluate earth pressure coefficients due to soil weight, vertical surcharge loading, and soil cohesion for the case of an inclined wall and sloping cohesionless backfill [21]. KΓΆtterβs [22] equation was suitably used to determine the point of application of active thrust by taking moments of all the forces and reaction about the base of the retaining wall [23]. A method was proposed by Kame et al. [24] to determine the active earth pressure and its point of application on a vertical wall retaining horizontal cohesionless backfill based on log-spiral failure mechanism coupled with KΓΆtterβs equation. Dewaikar et al. [25] used KΓΆtterβs equation to evaluate the magnitude of active thrust on an inclined wall retaining horizontal cohesionless backfill with uniform surcharge and to find out the point of application of reaction on the failure surface.
The objective of this study is to present a mathematical approach with a high degree of simplicity for the evaluation of the active thrust and its point of application. The analysis considers the free body diagram of the retaining wall in a very simple and analytical procedure and is easier for engineering application. The validity of the proposed approach is checked with previous available results.
2. Analysis of Active Thrust
The active thrust, , is determined from the conditions of force equilibrium and its point of application is determined from the conditions of moment equilibrium. Figure 1 shows an inclined retaining wall, with inclined cohesionless backfill subjected to a uniform surcharge intensity of q KN/m2. A trial plane failure surface [1] is considered which meets the ground surface at an angle, Ξ± with the horizontal. The trial wedge ABC is in equilibrium under the effect of three different forces: the equivalent force of the surcharge, W the soil reaction, R along the face trial failure BC, at an angle to the normal on BC and the active thrust , at an angle to the normal on the back.
The symbols used in Figure 1 are defined as follows.β: active thrust.β: equivalent force of the surcharge.β: soil reaction on the failure wedge.β: height of the retaining wall.β: height of point of application of active thrust from the wall base.β: inclination of the retaining wall with the horizontal.β: friction angle between the wall and soil backfill.β: soil friction angle.β: inclination of the trial failure plane with the horizontal.β: intensity of surcharge inβkN/m2.
Equating all the forces in the vertical and horizontal direction, the following force equilibrium conditions are obtained.
Horizontal force equilibrium:
from which R is obtained as
Vertical force equilibrium:
substituting the value of R from (2) into (3)
From (5), is obtained as
Now, applying sine rule to the triangle CAN,
or
Referring to Figure 1,
Substituting the value of AN in (8), AC is obtained as,
Substituting the value of AC in (6), the magnitude of active thrust is expressed as
The maximum value of active thrust is obtained when the inclination of the failure plane, BC, with the horizontal reaches the critical value, .
3. Evaluation of Soil Reaction on the Failure Surface
In a cohesionless soil medium with active state of equilibrium under plane strain condition, KΓΆtterβs [22] equation is given as (Figure 2)
whereβ: differential reactive pressure at a point on the failure surface,β: elemental length of the failure surface,β: angle made by the tangent at the point of interest with the horizontal,β: soil friction angle and,β: soil unit weight.
In the present analysis, only surcharge effect is taken into consideration, and therefore becomes zero. With this consideration (12) can be written as or For a plane failure surface, is zero and the corresponding solution for the reactive pressure, , is obtained as The above solution indicates that soil reactive pressure is uniformly distributed along the failure plane, BC. Therefore, the resultant soil reaction, R, acts at the mid-point of the failure plane, BC. The magnitude of soil reaction is computed after knowing the critical value, , of the angle, . Substituting the value of from (11) in to (2), the soil reaction R on the failure surface is obtained as
4. Point of Application of the Active Thrust
After obtaining the value of , the condition of moment equilibrium is applied. Figure 3 shows the free body diagram of the failure wedge ABC. The equivalent force of surcharge on the trial wedge, ABC, is , which acts at the midpoint of AC, that is, at a distance Y from the vertical line passing through the base the wall. As the distribution of reaction is uniform along the failure surface, it acts at the mid-point of the failure plane BC. The moments of all forces and reactions are taken about the base of the wall, at point B.
Moment equilibrium condition:
The surcharge acts at the center of AC with the distance Y given as,
where
From triangle AMP,
Now, substituting the value of AC from (10) and AP from (20) in (19) (Figure 3), is obtained as
Substituting the value of from (21) into (18), the point of application of equivalent surcharge force from the axis BM (Figure 3) is computed as
The soil reaction R acts at the midpoint of the failure plane BC, with the distance, (Figure 3), computed as
Referring to Figure 3, BC is obtained as
Substituting the value of BC from (24) and Y from (22) into (17), the distance X is obtained:
or
The height, , of point of application of from the wall base is obtained as
The coefficient of active earth pressure for the retaining wall with the surcharge effect is obtained as
5. Results and Discussions
One of the aims of the proposed analysis is the determination of point of application of the active thrust in a nondimensional form with the consideration of effect of various parameters. The height, , of point of application of the active thrust due to surcharge effect is expressed in a nondimensional form, , expressed as . The results are reported as shown in Table 1 along with figures that are described below.
In Figures 4 and 5, variation of with the angle of wall back, , is shown for and and 0.6 respectively. It is seen that , decreases with increasing angle of wall back and increases with increasing soil friction angle, .
In Figures 6, 7, and 8, variation of with the angle of backfill slope, Ξ², with is shown for ΞΈ = 65Β°, 70Β°, and 75Β°, respectively. It is seen that , increases with increasing Ξ², with higher values for higher soil friction angle, .
In Figure 9, variation of with the angle of wall friction, , is shown for 16Β° and Ο = 40Β°. It is seen that increases with , with higher values for higher .
In Figure 10 is shown the variation of for a vertical wall ( = 90Β°) and . It is again seen that increases with increase of .
In Figure 11, variation of with angle of soil friction, , is shown for a retaining wall with angle of wall back, ΞΈ = 90Β°, backfill slope, Ξ² = 0Β°, and angle of wall friction, Ξ΄ = 0Β°. It is interesting to note that is a constant value of 0.5 for all values of angle of soil friction, . Hence, the point of application of active thrust acts at the mid-height of a smooth vertical retaining wall with horizontal backfill.
The other aim of the proposed analysis is to compute the values of the active earth pressure coefficient, , for the various combinations of parameters considered in the analysis and compare the results with the available solution reported by Soubra and Macuh [21]. The results are presented through figures. In Figures 12, 13, and 14, the variation of active earth pressure coefficient, with angle of soil friction, is shown for , 0.6Ο, and 0.8Ο, respectively, for various values of angle of wall back, and . It is seen that values decrease with increasing angle of soil friction, . It is further seen that the values show an increasing trend with decreasing values of angle of wall back, .
In Figure 15 and Table 2 is shown the comparison of active earth pressure coefficients obtained from the proposed method and the method proposed by Soubra and Macuh [21]. The values obtained from the proposed method are higher with the maximum difference of 7.57% for the angle of wall back of 80Β°, Ο β€ 40Β°, and as shown in Table 2. For lower values of soil friction angle, , and angle of backfill slope, Ξ², the difference between the two results is less, showing an increasing trend with increasing angle of soil friction, , and backfill slope, .
6. Conclusions
The complete solution to a retaining wall problem is obtained only when the point of application of active thrust is known. KΓΆtterβs [22] equation lends itself as a powerful tool in the proposed analysis to determine the reactive pressure distribution on the failure plane. The moment equilibrium condition is used effectively to compute the point of application of the active thrust. From the proposed analysis it is seen that the point of application of the active thrust depends upon a number of factors such as angle of soil friction, , angle of wall friction, , angle of wall back, , and inclination of backfill, . It shows a wide variation in the range, 0.427 to 0.814. Only for the case of a smooth vertical wall retaining horizontal backfill, the point of application of the active thrust is at the wall mid-height. The present approach is easy to adapt for retaining walls and the results obtained based on this analysis are in fairly good agreement with other results.