Research ArticleEvaluation of Induced Settlements of Piled Rafts inthe Coupled Static-Dynamic Loads Using Neural Networks andEvolutionary Polynomial Regression
Ali Ghorbani andMostafa Firouzi Niavol
Department of Civil Engineering, Faculty of Engineering, The University of Guilan, Rasht, Iran
Correspondence should be addressed to Ali Ghorbani; [email protected]
Received 30 January 2017; Revised 27 April 2017; Accepted 6 June 2017; Published 19 July 2017
Academic Editor: Sandeep Chaudhary
Copyright © 2017 Ali Ghorbani and Mostafa Firouzi Niavol.This is an open access article distributed under theCreative CommonsAttribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work isproperly cited.
Coupled Piled Raft Foundations (CPRFs) are broadly applied to share heavy loads of superstructures between piles and raftsand reduce total and differential settlements. Settlements induced by static/coupled static-dynamic loads are one of the mainconcerns of engineers in designingCPRFs. Evaluation of induced settlements of CPRFs has been commonly carried out using three-dimensional finite element/finite difference modeling or through expensive real-scale/prototype model tests. Since the analyses,especially in the case of coupled static-dynamic loads, are not simply conducted, this paper presents two practical methods to gainthe values of settlement. First, different nonlinear finite differencemodels under different static and coupled static-dynamic loads aredeveloped to calculate exerted settlements. Analyses are performed with respect to different axial loads and pile’s configurations,numbers, lengths, diameters, and spacing for both loading cases. Based on the results of well-validated three-dimensional finitedifferencemodeling, artificial neural networks and evolutionary polynomial regressions are then applied and introduced as capablemethods to accurately present both static and coupled static-dynamic settlements. Also, using a sensitivity analysis based on CosineAmplitude Method, axial load is introduced as the most influential parameter, while the ratio l/d is reported as the least effectiveparameter on the settlements of CPRFs.
1. Introduction
CPRF is representative for combined piled raft foundation,which is commonly applied to suffer the heavy load ofskyscrapers through sharing the exerted load between raftand piles. Coefficient of piled raft, 𝛼pr, controls load sharingratio and is defined as the ratio of the sum of the loads carriedby piles to the corresponding value of the resistance of thewhole system. It varies from 0 for spread footings to 1 for pilefoundations. Also, as shown in Figure 1, the settlements of aCPRF (𝑆pr) can be calculated based on the value of (𝛼pr) andthe settlement of pile foundation (𝑆pf ).
Piles are generally used to decrease the foundation’stotal settlements. In the last three decades, some researcherslike those of [1–3] have declared efficient load sharingmechanisms to accurately investigate the piled raft behavior.
New well-developed computational approaches and availablefinite element (FE) codes such asDefpig andNapra have facil-itatedmodeling of available interactions [4–6]. Besides, someother small scale model studies [7, 8] and numerical and ana-lytical simulations in the literature have made improvementsin the design process [9–11]. In addition, results ofmonitoringthe behavior of piled rafts supporting heavy loads of someskyscrapers are reported [12, 13]. But there is an obvious needfor a comprehensive study about the piled raft settlementsin the case of combined vertical static loads and horizontaldynamic ones. Since it is experimentally time-consumingand expensive, numerical modeling is considered as a goodalternative to accurately study CPRFs behavior. However, inorder to have a comprehensive and accuratemodel, especiallyin the case of CPRFs for high rise buildingswith large numberof piles, there will be a large number of structural elements
HindawiApplied Computational Intelligence and So ComputingVolume 2017, Article ID 7487438, 23 pageshttps://doi.org/10.1155/2017/7487438
2 Applied Computational Intelligence and Soft Computing
Combined pile ra� foundation
JL
SJL/SM@
0.0
0.0
1.0
1.0
Figure 1: Settlement of a CPRF.
and the calculation time makes the analysis so difficult. Tocope with this difficulty, recently, some research works arefocused on the application of soft computing techniques, asthe speedy and powerful tool and alternative for other time-consuming and expensive methods, to the problem of pilesand piled raft foundations behaviors [14, 15]. In the researchof Armaghani et al. (2015) [14], the ultimate bearing capacityis investigated, while Baziar et al. (2014) [15] evaluated thestatic induced settlements. Hence, the dynamically loadedinduced settlements of piled rafts and the application ofsoft computing techniques to this problem have not beencompletely studied. Then, there is an obvious need for aspeedy and accurate tool for predicting piled raft settlementsin the combined vertical static-horizontal dynamic loadingconditions. Relying on the fact that conducting real-scale orprototype scale field or experimental tests on the dynamicbehavior of Coupled Piled Raft Foundations needs a lot oftime andmoney and also considering the process and analysistime of numerical modeling, if an alternative method forpredicting the settlements of CPRFs in dynamic loadingcases exists, it will be useful. This method should haveadvantages of both accurate experimental modeling and lowcalculation time. Hence, the application of neural networkmodeling and evolutionary polynomial regressions (EPRs),which are believed to be common ways to accurately andtimely predict engineering complicated functions, can beexamined. Different attempts to apply neural networks andEPRs to model different civil and geotechnical problems arepresented in the literature [14–33]. They are well-appliedin a wide range of problems from deep soil stabilizations,concrete, and their related structures, compressive strengthof soils, rocks, and stabilized samples, bearing capacityof shallow and deep foundations, lateral spreading, rockmechanics, rock engineering, and soil mechanics [14–33].In these methods, a sufficient amount of accurate data isrequired initially to train artificial neural networks andevolutionary polynomial regression models. In this regard,firstly, based on nonlinear dynamic finite difference method,piled raft foundationmodels were developed and successfullyvalidated with available field tests. Based on the parametricstudy on some geometrical parameters of CPRF and loads, acomprehensive sight to the problem has been achieved anda strong database has been prepared and results of induced
settlements for both static and coupled static-dynamic condi-tions are calculated and gathered regarding input concerningparameters. Then, using new powerful forecasting methods,for example, neural network modeling and evolutionarypolynomial regression modeling, it has been attempted topresent comprehensive, speedy, and accurate models forpredicting CPRF’s settlements in static and combined static-dynamic loading conditions. Hence, as the novelty of thepaper, new neural network and EPR models are presentedfor modeling settlements of CPRF in the static and coupledstatic-dynamic loading conditions. As another main resultof the paper, the most and the least influential parameters,which, respectively, should be paid more and less attentionsin dynamic CPRF modeling, are introduced.
2. Nonlinear Finite DifferenceModeling of CPRF
In order to develop CPRF models, FLAC 3D software wasused and CPRFs with regular 3 × 3, 4 × 4, and 5 × 5arrangements were modeled in both static and combinedstatic-dynamic conditions.
In order to achieve a comprehensive model, three differ-ent arrangements and topologies were considered for piles(pattern N for near piles, pattern M for mediate piles, andpattern F for far piles). Also, 4, 5, and 6 were the ratios of 𝑆/𝐷(spacing of piles to the piles’ diameters). Also, assuming four(𝑙/𝐷) conditions (16, 20, 24, and 32) and two different staticvertical pressure states (60 and 90 kPa) static and combinedstatic-dynamic settlements were calculated.
In order tomodel three-dimensional soil and pile geome-try, 8-node brick elements and 6-node cylinder elements are,respectively, used. Names, shapes and other specifications ofthe used mesh shapes are presented in Figure 2.
Also, there are some well-developed constitutive modelspresented in FLAC as built in material behaviors. Amongthem, Mohr-Coulomb’s model applies more simple constitu-tive parameters (in view of characterization), internal fric-tion angle, cohesion, and dilation. Hence, it is considerablyapplied to model the behavior of surrounding soil. Also,in order to investigate the interaction between the soil andpiles, shear and normal coupling springs are used. In thispaper, using nonassociativeMohr-Coulombmodel (the yieldsurface is presented in Figure 3), the soil nonlinear behavioris modeled, while slippage and separation during the motionare described using coupling springs. The normal behaviorof the pile/grid interface is represented by a spring with alimiting normal force, which is dependent on the directionof piles’ nodal movement. In addition, the shear behaviorof the pile/grid interface is represented as a spring-slidersystem at the nodes of modeled piles. The shear behavior ofthe interface during relative displacement between the nodalpoints of pile and the grid is numerically attained by adjustingthe proper shear and normal stiff-nesses. Elements of theinterface and parameters of the used constitutivemodel in theinterface along with the interface elements along the bottomand the side are presented in Figure 4.
Applied Computational Intelligence and Soft Computing 3
Shape Name Keyword Referencepoints
Sizeentries
Dimensionentries Fill
No038
037
036
036
035
034
036
BrickBrick
Degeneratebrick
Wedge
Uniformwedge
Pyramid
Tetrahedron
Cylinder
Dbrick
Wedge
Uwedge
Pyramid
Tetrahedron
Cylinder
No
No
No
No
No
No
Figure 2: Specifications of the used elements [16].
−�휎3
−�휎1
−�휎2
�휎1= �휎2
= �휎3Mohr-Coulomb �휙 > 0
Tresca �휙 = 0√3C cot �휙
Figure 3: Mohr-Coulomb material model used to investigate thenonlinear soil behavior [6].
For the analysis of the piled raft foundation, the soilas well as the structure is discretized into elements. Usualpractice is to divide the soil mass into rectangular zonesof aspect ratios less than 4 : 1. For the region of greaterinterest, finer discretization is used. The software internallybreaks each of the rectangular elements into four overlappingtriangular elements. The limits of the discretized grid shouldbe properly planned to suit the geometry of the problem. Toavoid boundary effects, the mesh should extend sufficientlybeyond the region of interest. Experiences of the previousresearchers are taken as guidelines to decide the extent of thegrid. The software also allows graded discretization, whichis more efficient than abrupt change in zone sizes. In thisregard, a sensitivity analysis on the number of grids (meshrefinement) is conducted to obtain the proper mesh size, inwhich the size of elements does not meaningfully change theaccuracy of results. Figure 5 presents the adopted mesh forpiles cap and the soil and the pile’s length in the optimumrefined mesh view. A typical shape for one of the developed
models has been shown in Figure 6, where elements near thepiles are finer than others to accurately track the sensitivitiesin this zone (with higher stress intensity). In addition, inorder to neglect the boundary effects, the lateral boundariesare in the distances equal to 50𝐷 from the edge of raft.Moreover, the distance between lower boundaries with the tipof piles is assumed to be 3𝐿 (length of piles). It should be notedthat interactions between soil and piles have been accuratelyconsidered using interface elements and [34]
𝑘𝑠 = 𝑘𝑛 = 10max(𝐾 + 4/3𝐺Δ𝑧min) , (1)
where𝐾 is the soil’s bulk modulus, 𝐺 is the shear modulus ofthe soil, Δ𝑧min is the minimum width of neighbor elementsat the interface, and 𝑘𝑠 and 𝑘𝑛, respectively, present shear andnormal stiffness of elements at interface nodes.
2.1. Dynamic Analysis. Critical time step is calculated using[34]
Δ𝑡crit = min{ 𝐴𝐶𝑃Δ𝑥max} , (2)
where 𝐶𝑝 is the speed of 𝑃 wave, 𝐴 represents the area oftriangular element, and Δ𝑥max is the maximum dimension ofthe area. In the case of damping proportional to the stiffness,the critical time step is calculated using [36]
Δ𝑡𝛽 = { 2𝜔max} (√1 + 𝜆2 − 𝜆) , (3)
4 Applied Computational Intelligence and Soft Computing
Interface node Interface element
Node’s representative area
(a)
Target face
Ss S ks
Ts
D
kn
P
S = SliderTs = Tensile strengthSs = Shear strength
D = Dilationks = Shear sti�nesskn = Normal sti�ness
(b)
r_pael 1 r_pael 2
H_pael 1H_pael 2
Interface along sidesInterface at bottom
x
y
z
(c)
Figure 4: (a) Interface elements; (b) constitutive parameters in the interface; (c) bottom and side interface elements [16].
where 𝜔max is maximum predominant frequency of systemand 𝜆 represents a ratio of critical damping at this frequencyand are calculated using [34]
𝜔max = 2Δ𝑡𝑑 ,
𝜆 = 0.4𝛽Δ𝑡𝑑 ,𝛽 = 𝜉min𝜔min
.(4)
Applied Computational Intelligence and Soft Computing 5
Figure 5: Two different grid sizes used to carry out the sensitivity analysis on the mesh sizes.
D
S/2
S/2
S
Figure 6: Developed three-dimensional FD model.
In these equations, 𝜉min and 𝜔min are Rayleigh’s damping andangular frequency.
2.2. Boundary Conditions. Quiet boundaries introduced byLysmer and Kuhlemeyer [34] are used to neglect the effectsof wave reflections in the model. In these boundaries, normaland shear quiet tensions are modeled using [34]
𝑡𝑛 = −𝜌𝐶𝑃𝜐𝑛,𝑡𝑆 = −𝜌𝐶𝑆𝜐𝑆, (5)
where 𝜐𝑛 and 𝜐𝑆 are, respectively, normal and shear com-ponents of wave velocity at boundary. 𝜌 is specific gravityand 𝐶𝑃 and 𝐶𝑆 represent 𝑃 and 𝑆 wave’s speed, respectively.Also, 𝑡𝑛 and 𝑡𝑆, respectively, show the normal and shear quiettensions. Figure 7 shows quiet boundaries used in FLAC forrigid and flexible beds.
2.3. Loading Condition. As mentioned, in order to evaluatethe effect of coupled vertical static loading and horizontaldynamic loading, 60 and 90 kPa vertical loadswere separatelyexerted to the structure and the model was analyzed. Also,dynamic loading was modeled using horizontal stress waveas shown in Figure 8. Since quiet boundaries were used,acceleration/speed time histories at boundaries cannot beexerted to the models. Hence, based on (6) [34], the wavevelocities were changed to the waves’ stress terms and shownin Figure 8.
𝜎𝑛 = 2 (𝜌𝐶𝑃) 𝜐𝑛,𝜎𝑆 = 2 (𝜌𝐶𝑆) 𝜐𝑆, (6)
where 𝜐𝑛 and 𝜐𝑆 are, respectively, normal and shear compo-nents of the wave velocity at boundary. 𝜌 is specific gravityand 𝐶𝑃 and 𝐶𝑆 represent 𝑃 and 𝑆 wave’s velocity, respectively.
6 Applied Computational Intelligence and Soft Computing
Free
�el
d
Free
�el
d
Structure
Internaldynamic
input
External dynamic input (stress or force only)
Quiet boundary
Qui
et b
ound
ary
Qui
et b
ound
ary
3Ddamping
(a)
Free
�el
d
Free
�el
d
Structure
Internaldynamic
input
External dynamic input (acceleration or velocity)
Qui
et b
ound
ary
Qui
et b
ound
ary
3Ddamping
(b)
Figure 7: Quiet boundaries for (a) rigid and (b) flexible beds in FLAC 3D [16].
0 1 2 3 4 5 6 7 8 9 10
Time (s)−25−20−15−10−5
05
10152025
Stre
ss (k
Pa)
Figure 8: Exerted horizontal stress wave.
3. Validation of Numerical Model
In order to further study and investigate the role of each of theconcerning parameters, the previously well-validated three-dimensional finite differencemodeling procedure (previouslyapplied by the corresponding author of the paper) is used [6].This model was validated using a 1 g physical model test onmedium dense sand with the soil and pile geometry shownin Figure 9. In addition, the adopted mesh along with thecomparison of physical modeling results with the results ofnumerical modeling are also shown in Figure 9. As it can beseen, there is an acceptable agreement between the results ofthree-dimensional nonlinear finite difference modeling and1 g physical modeling [6].
4. Parametric Study on FiniteDifference Model
As it wasmentioned, the effect of some of the geometrical pileparameters and the loads on the static and combined static-dynamic CPRF’s settlements has been studied. Consideringthree pile patterns (different configurations), two differentpile diameters, three ratios for 𝑠/𝑑, four ratios for 𝑙/𝑑, andtwo different static load states, a databank with 144 staticdata series and 144 dynamic ones has been achieved. Figures
10 and 11 show the results of static and combined static-dynamic settlements for the 3 × 3 CPRF as a sample of theresults. As shown, F-architecture is the best architecture, inwhich the minimum settlements are observed in both staticand coupled static-dynamic models. Besides, increasing 𝑠/𝑑ratio will result in an increase in the calculated settlements.However, piles with larger lengths cause smaller inducedstatic and coupled static-dynamic settlements.The combinedeffects of 𝑠/𝑑 and 𝑙/𝑑 can be better tracked using a sensitivityanalysis. The following sections present the sensitivity anal-ysis, which shows the relative importance of increasing 𝑙/𝑑and decreasing 𝑠/𝑑 in the reduction of induced settlements.As shown and comparing to the effect of increasing 𝑙/𝑑ratio, decreasing s/d ratio plays more important role in thereduction of the settlements in both cases.
Furthermore, Tables 1 and 2, respectively, present theresults of parametric study on the whole affecting parametersfor static loading condition and combined static-dynamicloading condition.
The following subsections present parametric studiesconducted on different concerning parameters (e.g., piles’lengths, diameters, spacing, architecture, and axial loads). Inthis regard and as sample cases, settlements of CPRFs undercoupled static-dynamic loads are presented and discussed fordifferent parameters.
4.1. Effect of Piles’ Architecture (Pattern) on the Settlementsof CPRF. To investigate the effect of piles’ arrangement andtheir architecture on the static and coupled static-dynamicsettlements, three different patterns are considered, where N,F, and M symbols stand for the near-, far-, and medium-distance piles architectures, respectively. As described, 0.3and 0.5 meters are the values of piles’ diameter used tocalculate the induced settlements. In this section, effects ofdifferent piles’ architectures on the coupled static-dynamicsettlements of 0.5meters in diameter piles under 60 kPa staticaxial load are evaluated. Figure 12(a) shows coupled static-dynamic settlements of the studied 3 ∗ 3-CPRF for N, F, andM arrangements. Also, Figures 12(b) and 12(c), respectively,present corresponding results for 4 ∗ 4 and 5 ∗ 5 CPRFs. It
Applied Computational Intelligence and Soft Computing 7
y
y
x
x
D
SSS/2
D/2
D/2
d/2 d
t
S
H
1.77D
S/2
D = 220S = 70d = 25
H = 1000t = 40
Lp = 550
Lp
(a) (b)
1 g testPresent numerical methodPDR
0 5 10 15 20Load (KN)
30
25
20
15
10
5
0
Settl
emen
t (m
m)
(c)
Figure 9: (a) Geometry of conducted physical model. (b) Three-dimensional finite difference mesh. (c) Comparison of the results of finitedifference and physical model [6].
8 Applied Computational Intelligence and Soft Computing
Table 1: Parametric study on the whole affecting parameters for static loading condition.
Number of piles 𝑑 (m) 𝑠/𝑑 𝑙/𝑑 𝑝 (kPa) 𝑆 (cm)Mean: 16.67 Mean: 0.4 Mean: 5 Mean: 23 Mean: 75 Mean: 5.96Std. Dev.: 6.57 Std. Dev.: 0.1 Std. Dev.: 0.82 Std. Dev.: 5.94 Std. Dev.: 15.05 Std. Dev.: 1.729 0.3 4 16 90 8.329 0.3 4 20 90 7.239 0.3 4 24 90 6.099 0.3 4 32 90 59 0.3 5 16 90 7.529 0.3 5 20 90 6.529 0.3 5 24 90 5.259 0.3 5 32 90 4.239 0.3 6 16 90 7.129 0.3 6 20 90 6.119 0.3 6 24 90 5.019 0.3 6 32 90 49 0.3 4 16 60 5.839 0.3 4 20 60 5.039 0.3 4 24 60 4.319 0.3 4 32 60 3.59 0.3 5 16 60 5.329 0.3 5 20 60 4.669 0.3 5 24 60 3.719 0.3 5 32 60 2.9619 0.3 6 16 60 5.029 0.3 6 20 60 4.319 0.3 6 24 60 3.519 0.3 6 32 60 2.816 0.3 4 16 90 9.15216 0.3 4 20 90 7.95316 0.3 4 24 90 6.69916 0.3 4 32 90 5.516 0.3 5 16 90 8.27216 0.3 5 20 90 7.17216 0.3 5 24 90 5.77516 0.3 5 32 90 4.65316 0.3 6 16 90 7.83216 0.3 6 20 90 6.7216 0.3 6 24 90 5.5116 0.3 6 32 90 4.416 0.3 4 16 60 6.86416 0.3 4 20 60 5.9647516 0.3 4 24 60 5.0216 0.3 4 32 60 4.12516 0.3 5 16 60 6.20416 0.3 5 20 60 5.3816 0.3 5 24 60 4.3316 0.3 5 32 60 3.4916 0.3 6 16 60 5.8716 0.3 6 20 60 5.0416 0.3 6 24 60 4.1316 0.3 6 32 60 3.325 0.3 4 16 90 9.9825 0.3 4 20 90 8.6725 0.3 4 24 90 7.3
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Table 1: Continued.
Number of piles 𝑑 (m) 𝑠/𝑑 𝑙/𝑑 𝑝 (kPa) 𝑆 (cm)Mean: 16.67 Mean: 0.4 Mean: 5 Mean: 23 Mean: 75 Mean: 5.96Std. Dev.: 6.57 Std. Dev.: 0.1 Std. Dev.: 0.82 Std. Dev.: 5.94 Std. Dev.: 15.05 Std. Dev.: 1.7225 0.3 4 32 90 5.99525 0.3 5 16 90 9.0225 0.3 5 20 90 7.8225 0.3 5 24 90 6.2925 0.3 5 32 90 5.0725 0.3 6 16 90 8.5425 0.3 6 20 90 7.3325 0.3 6 24 90 6.0125 0.3 6 32 90 4.825 0.3 4 16 60 7.7825 0.3 4 20 60 6.7625 0.3 4 24 60 5.725 0.3 4 32 60 4.6825 0.3 5 16 60 7.0325 0.3 5 20 60 6.125 0.3 5 24 60 4.9125 0.3 5 32 60 3.9625 0.3 6 16 60 6.6625 0.3 6 20 60 5.7125 0.3 6 24 60 4.6925 0.3 6 32 60 3.749 0.5 4 16 90 9.019 0.5 4 20 90 8.299 0.5 4 24 90 6.729 0.5 4 32 90 5.239 0.5 5 16 90 8.119 0.5 5 20 90 79 0.5 5 24 90 5.729 0.5 5 32 90 4.759 0.5 6 16 90 7.529 0.5 6 20 90 6.829 0.5 6 24 90 5.569 0.5 6 32 90 4.529 0.5 4 16 60 5.959 0.5 4 20 60 5.479 0.5 4 24 60 4.449 0.5 4 32 60 3.459 0.5 5 16 60 5.359 0.5 5 20 60 4.629 0.5 5 24 60 3.789 0.5 5 32 60 3.149 0.5 6 16 60 4.969 0.5 6 20 60 4.59 0.5 6 24 60 3.679 0.5 6 32 60 2.9816 0.5 4 16 90 9.7316 0.5 4 20 90 8.9516 0.5 4 24 90 7.2616 0.5 4 32 90 5.6516 0.5 5 16 90 8.7616 0.5 5 20 90 7.56
10 Applied Computational Intelligence and Soft Computing
Table 1: Continued.
Number of piles 𝑑 (m) 𝑠/𝑑 𝑙/𝑑 𝑝 (kPa) 𝑆 (cm)Mean: 16.67 Mean: 0.4 Mean: 5 Mean: 23 Mean: 75 Mean: 5.96Std. Dev.: 6.57 Std. Dev.: 0.1 Std. Dev.: 0.82 Std. Dev.: 5.94 Std. Dev.: 15.05 Std. Dev.: 1.7216 0.5 5 24 90 6.1816 0.5 5 32 90 5.1316 0.5 6 16 90 8.1216 0.5 6 20 90 7.3716 0.5 6 24 90 616 0.5 6 32 90 4.8816 0.5 4 16 60 6.8116 0.5 4 20 60 6.2716 0.5 4 24 60 5.0816 0.5 4 32 60 3.9516 0.5 5 16 60 6.1316 0.5 5 20 60 5.2916 0.5 5 24 60 4.3216 0.5 5 32 60 3.5916 0.5 6 16 60 5.6916 0.5 6 20 60 5.1616 0.5 6 24 60 4.216 0.5 6 32 60 3.4225 0.5 4 16 90 10.725 0.5 4 20 90 9.8525 0.5 4 24 90 7.9825 0.5 4 32 90 6.2125 0.5 5 16 90 9.6325 0.5 5 20 90 8.3225 0.5 5 24 90 6.825 0.5 5 32 90 5.6425 0.5 6 16 90 8.9325 0.5 6 20 90 8.125 0.5 6 24 90 6.6125 0.5 6 32 90 5.3725 0.5 4 16 60 7.9225 0.5 4 20 60 7.2925 0.5 4 24 60 5.9125 0.5 4 32 60 4.625 0.5 5 16 60 7.1325 0.5 5 20 60 6.1525 0.5 5 24 60 5.0325 0.5 5 32 60 4.1825 0.5 6 16 60 6.6125 0.5 6 20 60 625 0.5 6 24 60 4.8925 0.5 6 32 60 3.97
should be noted that the reported value for the settlement ofeach CPRF is the average of pile tip’s settlement since a rigidbehavior is assumed for the piles’ cap.
As shown, N-architecture CPRFs experience the largestsettlements, while F-architecture shows a better resistanceagainst settlements. This is because of the piles group’s
performance in the CPRF. Indeed, in far-piles architecture(F), with decreasing the relative effect of piles, each individualpile behaves as a single pile and enhances the resistance of thewhole CPRF.Nevertheless, in theN-architecture, overlappingstress bubbles of individual piles, the maximum resistance ofthe whole CPRF against the settlement decreases.
Applied Computational Intelligence and Soft Computing 11
Table 2: Parametric study on the whole affecting parameters for combined static-dynamic loading condition.
Number of piles 𝑑 (m) 𝑠/𝑑 𝑙/𝑑 𝑝 (kPa) 𝑆 (cm)Mean: 16.67 Mean: 0.4 Mean: 5 Mean: 23 Mean: 75 Mean: 6.67Std. Dev.: 6.57 Std. Dev.: 0.1 Std. Dev.: 0.82 Std. Dev.: 5.94 Std. Dev.: 15.05 Std. Dev.: 2.219 0.3 4 16 90 10.8169 0.3 4 20 90 9.049 0.3 4 24 90 6.949 0.3 4 32 90 5.59 0.3 5 16 90 9.17449 0.3 5 20 90 7.769 0.3 5 24 90 5.789 0.3 5 32 90 4.489 0.3 6 16 90 8.47289 0.3 6 20 90 7.039 0.3 6 24 90 5.419 0.3 6 32 90 4.169 0.3 4 16 60 7.359 0.3 4 20 60 6.049 0.3 4 24 60 4.789 0.3 4 32 60 3.689 0.3 5 16 60 6.339 0.3 5 20 60 5.369 0.3 5 24 60 3.979 0.3 5 32 60 3.029 0.3 6 16 60 5.829 0.3 6 20 60 4.839 0.3 6 24 60 3.659 0.3 6 32 60 2.8316 0.3 4 16 90 11.6216 0.3 4 20 90 9.5416 0.3 4 24 90 7.3716 0.3 4 32 90 5.7816 0.3 5 16 90 9.9316 0.3 5 20 90 8.3216 0.3 5 24 90 6.2416 0.3 5 32 90 4.7916 0.3 6 16 90 9.1616 0.3 6 20 90 7.6616 0.3 6 24 90 5.6216 0.3 6 32 90 4.4416 0.3 4 16 60 8.6516 0.3 4 20 60 7.1616 0.3 4 24 60 5.5816 0.3 4 32 60 4.3316 0.3 5 16 60 7.3816 0.3 5 20 60 6.1916 0.3 5 24 60 4.6316 0.3 5 32 60 3.5616 0.3 6 16 60 6.8116 0.3 6 20 60 5.6516 0.3 6 24 60 4.316 0.3 6 32 60 3.3325 0.3 4 16 90 11.7725 0.3 4 20 90 9.88
12 Applied Computational Intelligence and Soft Computing
Table 2: Continued.
Number of piles 𝑑 (m) 𝑠/𝑑 𝑙/𝑑 𝑝 (kPa) 𝑆 (cm)Mean: 16.67 Mean: 0.4 Mean: 5 Mean: 23 Mean: 75 Mean: 6.67Std. Dev.: 6.57 Std. Dev.: 0.1 Std. Dev.: 0.82 Std. Dev.: 5.94 Std. Dev.: 15.05 Std. Dev.: 2.2125 0.3 4 24 90 8.0325 0.3 4 32 90 6.2925 0.3 5 16 90 10.3725 0.3 5 20 90 8.6825 0.3 5 24 90 6.825 0.3 5 32 90 5.2225 0.3 6 16 90 9.6525 0.3 6 20 90 8.0625 0.3 6 24 90 6.1325 0.3 6 32 90 4.8425 0.3 4 16 60 9.825 0.3 4 20 60 7.9125 0.3 4 24 60 6.3825 0.3 4 32 60 4.9125 0.3 5 16 60 8.3725 0.3 5 20 60 6.8325 0.3 5 24 60 5.3525 0.3 5 32 60 4.0425 0.3 6 16 60 7.6625 0.3 6 20 60 6.2925 0.3 6 24 60 4.8725 0.3 6 32 60 3.789 0.5 4 16 90 11.35269 0.5 4 20 90 9.79 0.5 4 24 90 7.469 0.5 4 32 90 5.659 0.5 5 16 90 9.65099 0.5 5 20 90 7.989 0.5 5 24 90 6.299 0.5 5 32 90 4.859 0.5 6 16 90 8.72329 0.5 6 20 90 7.59 0.5 6 24 90 5.849 0.5 6 32 90 4.579 0.5 4 16 60 7.29 0.5 4 20 60 6.49 0.5 4 24 60 4.839 0.5 4 32 60 3.629 0.5 5 16 60 6.169 0.5 5 20 60 5.179 0.5 5 24 60 3.969 0.5 5 32 60 3.29 0.5 6 16 60 5.719 0.5 6 20 60 4.959 0.5 6 24 60 3.749 0.5 6 32 60 3.0116 0.5 4 16 90 11.8716 0.5 4 20 90 10.5616 0.5 4 24 90 7.7716 0.5 4 32 90 5.93
Applied Computational Intelligence and Soft Computing 13
Table 2: Continued.
Number of piles 𝑑 (m) 𝑠/𝑑 𝑙/𝑑 𝑝 (kPa) 𝑆 (cm)Mean: 16.67 Mean: 0.4 Mean: 5 Mean: 23 Mean: 75 Mean: 6.67Std. Dev.: 6.57 Std. Dev.: 0.1 Std. Dev.: 0.82 Std. Dev.: 5.94 Std. Dev.: 15.05 Std. Dev.: 2.2116 0.5 5 16 90 10.2516 0.5 5 20 90 8.6916 0.5 5 24 90 6.4216 0.5 5 32 90 5.2816 0.5 6 16 90 9.4216 0.5 6 20 90 8.2516 0.5 6 24 90 6.1216 0.5 6 32 90 4.9316 0.5 4 16 60 8.2416 0.5 4 20 60 7.416 0.5 4 24 60 5.5916 0.5 4 32 60 4.1516 0.5 5 16 60 7.1116 0.5 5 20 60 5.9316 0.5 5 24 60 4.5416 0.5 5 32 60 3.6616 0.5 6 16 60 6.5416 0.5 6 20 60 5.6716 0.5 6 24 60 4.3716 0.5 6 32 60 3.4525 0.5 4 16 90 12.3125 0.5 4 20 90 10.8325 0.5 4 24 90 8.4625 0.5 4 32 90 6.3425 0.5 5 16 90 10.7925 0.5 5 20 90 9.2325 0.5 5 24 90 7.1425 0.5 5 32 90 5.8125 0.5 6 16 90 10.0125 0.5 6 20 90 8.5925 0.5 6 24 90 6.7425 0.5 6 32 90 5.4225 0.5 4 16 60 9.5825 0.5 4 20 60 8.3825 0.5 4 24 60 6.525 0.5 4 32 60 4.6925 0.5 5 16 60 8.2725 0.5 5 20 60 6.7725 0.5 5 24 60 5.3325 0.5 5 32 60 4.2625 0.5 6 16 60 7.4725 0.5 6 20 60 6.4825 0.5 6 24 60 4.9925 0.5 6 32 60 4.01
14 Applied Computational Intelligence and Soft Computing
Pattern F Pattern M Pattern NPattern
3.5
4
4.5
5
5.5
6
6.5
7
7.5
8
8.5
Settl
emen
t (cm
)
L = 4.8 mL = 6 m
L = 7.2 mL = 9.6 m
Figure 10: Static CPRF’s settlements at 90 kPa overburden.
Pattern F Pattern M Pattern NPattern
3.5
4.5
5.5
6.5
7.5
8.5
9.5
10.5
11.5
Settl
emen
t (cm
)
L = 4.8 mL = 6 m
L = 7.2 mL = 9.6 m
Figure 11: CPRF’s settlements under combined static (90 kPa)-dynamic load.
4.2. Effect of Pile’s Length on the Settlements of CPRF. To showthe effect of piles’ length, as sample results, settlements ofdifferent CPRFs are shown in Figure 13. Figures 13(a), 13(b),and 13(c), respectively, describe the effect of piles’ length onthe coupled static-dynamic settlements of the studied 3 ∗ 3,4 ∗ 4, and 5 ∗ 5 CPRFs under 60 kPa static axial load for 0.5meters in diameter piles.
It is seen that, for a constant architecture, with increasingthe length of piles, value of coupled static-dynamic settle-ments decreases.
4.3. Effect of Axial Pile Loads on the Settlements of CPRF.In this section, as a sample case, settlements of a 3 ∗ 3-architecture CPRF (with constant diameter piles, 𝑑 = 0.5m)under 60 kPa and 90 kPa static axial force subjected to ahorizontal dynamic load are evaluated. As shown in Figure 14,the value of axial force affects the induced settlements. Itis observed that, with increasing the static axial force, theinduced settlements increase.
5. Artificial Intelligence Techniques
5.1. Artificial Neural Networks. Artificial Intelligence hasdifferent branches. Among these branches, Artificial NeuralNetworks (ANNs) are known as the black box, while Evo-lutionary Polynomial regression (EPR) is referred to as thegrey box method. In ANNs, generally, experimental datasetsare used to attain relationships between input and outputparameters. In this method, the large number of databasesis one of the requirements to get the results with less error[17–22, 37].
The relationship between input and output parametersis gained using the learning rules. In spite of classicalstatisticalmethods, neural networks donot need any previousknowledge about the quality and mechanics of the problemand their concerning parameters. One of themost in-demandkinds of neural networks is multilayer perceptron (MLP)networks, which is formed using correct definition of itsconstructing layers, input, and hidden and output layers[23]. Regarding the type of problem complexity and itsnonlinearity, the number of MLP layers is defined [24].The constructing elements of each layer are neurons, whichare connected to the neurons of other layers, but cannotmake connection with the neurons of the same layer. Therelationship between neurons of a layer to the neurons of thenext neighboring layer is carried out using some connections.The analyzed information will be multiplied to the assignedweight of each node and then will be transformed using theactivation function [38]. In an MLP, as shown in Figure 15,independent input variables are connected to the neuronsof hidden layers and can predict the multiple dependentoutput variables based on network training (by detectingthe similarities between input and output parameters andminimizing the prediction errors) [25]. Hence, architectureof the network, learning rule, and the transfer function arekey parameters, which should be correctly defined to build aproper neural network [35].
5.1.1. Neural Network Training. Feed-Forward Backpropaga-tion, FFBP, is the most applied algorithm used to train theneural networks for a broad range of engineering applications[26]. In this training algorithm, firstly and in forward pass,assuming a primary value for connection between neurons,outputs are forecasted and then the computational error iscalculated. This error will be backcalculated to update the
Applied Computational Intelligence and Soft Computing 15
Pattern FPattern MPattern N
2.5
3.5
4.5
5.5
6.5
7.5
Settl
emen
t (cm
)
1 2 3 4 50Pile length (m)
(a) 3 ∗ 3 piles
Pattern FPattern MPattern N
3
4
5
6
7
8
9
Settl
emen
t (cm
)
1 2 3 4 50Pile length (m)
(b) 4 ∗ 4 piles
Pattern FPattern MPattern N
3.5
4.5
5.5
6.5
7.5
8.5
9.5
10.5
Settl
emen
t (cm
)
1 2 3 4 50Pile length (m)
(c) 5 ∗ 5 piles
Figure 12: Effect of piles’ architecture on the coupled static-dynamic settlements of CPRF (𝑑 = 0.5m, 𝑝 = 60 kPa).
neuron’s weights and obtain accurate outputs. This secondphase is called backpropagation phase [27].
In order to make all the input and output parametersdimensionless, (7) [28, 29] is used and all the parameters arenormalized to a 0-1 scale.
Scaled Parameter
= (unscaled parameter − parameter’s min. value)(parameter’s max. value − parameter’s min. value) .
(7)
In this paper, training and cross-validation datasets weremade through random selection of 85%of thewhole data.Theremaining 15% are the testing data series. Different transferfunctions, for example, TANSIG, LOGSIG, and PURELIN,are available to be used as the transfer function to mathemat-ically represent, in terms of spatial or temporal frequency, therelation between the input and output.The transfer functionsusually have a sigmoid shape, but they may also take theformof other nonlinear functions, piecewise linear functions,or step functions. Hence, to evaluate the ability of different
16 Applied Computational Intelligence and Soft Computing
Pattern F Pattern M Pattern NPattern
2.5
3
3.5
4
4.5
5
5.5
6
6.5
7
7.5Se
ttlem
ent (
cm)
L = 4.8 mL = 6 m
L = 7.2 mL = 9.6 m
(a) 3 ∗ 3 piles
Pattern F Pattern M Pattern NPattern
3
4
5
6
7
8
9
Settl
emen
t (cm
)
L = 4.8 mL = 6 m
L = 7.2 mL = 9.6 m
(b) 4 ∗ 4 piles
Pattern F Pattern M Pattern NPattern
3.5
4.5
5.5
6.5
7.5
8.5
9.5
10.5
Settl
emen
t (cm
)
L = 4.8 mL = 6 m
L = 7.2 mL = 9.6 m
(c) 5 ∗ 5 piles
Figure 13: Effect of piles’ length on the coupled static-dynamic settlements of CPRF (𝑑 = 0.5m, 𝑝 = 60 kPa).
transfer functions in the prediction of coupled static-dynamicCPRF’s settlements, the mentioned transfer functions wereapplied and TANSIG function showing the best performancewas selected for the modeling purposes. Figure 16 shows theTANSIG transfer function. Also, (8) shows the formula usedto calculate TANSIG function [39].
𝑓 = 𝑒𝑒𝑥 − 𝑒−𝑒𝑥𝑒𝑒𝑥 + 𝑒−𝑒𝑥 , (8)
where 𝑒𝑥 represents the weighted sum for each of theconcerning input parameters [39].
In addition, underfitting and overfitting should beavoided during constructing the networks. Indeed, usingincorrect number of solution epochs leads to these twophenomena. Overfitting corresponds to the case of too manytraining cycles, while underfitting declares that insufficientepochs are used to train the network [30].
5.2. Evolutionary Polynomial Regression Modeling. Evolu-tionary Polynomial Regression (EPR) modeling simulta-neously uses the advantages of both numerical regressionanalysis and the genetic programing. It applies the least
Applied Computational Intelligence and Soft Computing 17
Pattern F Pattern M Pattern NPattern
2.5
3
3.5
4
4.5
5
5.5
6
6.5
7
7.5Se
ttlem
ent (
cm)
L = 4.8 mL = 6 m
L = 7.2 mL = 9.6 m
(a) 𝑝 = 60 kPa
Pattern F Pattern M Pattern NPattern
4
5
6
7
8
9
10
11
12
Settl
emen
t (cm
)
L = 4.8 mL = 6 m
L = 7.2 mL = 9.6 m
(b) 𝑝 = 90 kPa
Figure 14: Effect of axial load on the coupled static-dynamic settlements of CPRF (𝑑 = 0.5m, 3 ∗ 3 architecture).
N
r
s/d
l/d
P
S
Input Output
First hidden layer Second hidden layer
Figure 15: Multilayer perceptron neural network.
squares method to estimate the constants of a previouslyevolutionary developedmodel [40].The general steps appliedin EPR are depicted in Figure 17.
In this method, type of adopted functions, number ofterms exponents’ range, and the number of generations arethe parameters which affect the output relationship [31].Besides, similar to the neural network modeling, the coef-ficient of determination evaluates the degree of accuracy of
1
−1
0
n
a
a = Tansig (n)
Figure 16: Nonlinear TANSIG transfer function [34].
the proposed equation. If the proposed model satisfied bothtermination criteria (maximum number of generations andsentences) and required prediction accuracy, it will terminate.Otherwise, it goes through another evolution [32].
6. Results
In order to evaluate and compare the developed models andtechniques, their performances have been investigated indifferent various terms.
18 Applied Computational Intelligence and Soft Computing
Input matrix
Exponent vectors(random initiation population)
Population of mathematical structures(created by assigning exponent vectors to the corresponding input matrix)
Population of equations(least square method used to evaluate coe�cients)
�tness of the population equations is evaluated
Terminationcriteria
satis�ed?
Yes
No
Results
Individuals from matingpool selected
Exponent vectorselected
New generation ofexponent vector
GA
Figure 17: Typical flow diagram for EPR procedure [35].
6.1. Neural Network Modeling of Static and Coupled Static-Dynamic Loading Induced Settlement of CPRF
6.1.1. Architectures of the Best Neural Networks. Different one-and two-layered networks with different neurons for eachhidden layer were built and trained. In order to evaluatethe constructed networks, the value of root mean squarederror, RMSE, and the coefficient of determination, 𝑅2, werecalculated. For all the built models, the value of root meansquared error, RMSE, and mean absolute error and, also,coefficient of correlation, 𝑅2, were calculated and compared.The applied formula for calculating RMSE is presented in [29]
RMSE = √∑ (𝑂𝑖 − 𝑇𝑖)2𝑛 , (9)
where 𝑇𝑖 and 𝑂𝑖 are calculated and forecasted outputs,respectively. Also, 𝑛 is the number of datasets.
6.1.2. Neural Network Performances. To evaluate the perfor-mance of the optimum models, the normalized predictedvalues of static and combined static-dynamic settlements (fortesting data series) are predicted using both conventional andgenetic algorithm based neural networks.
(1) Performance of Neural Networks in the Static Loading Case.The value of RMSE and coefficient of correlation along withthe slope of fitting line, 𝐴, for different network architecturesare shown in Table 3, where different terms, digits, of each ofthe network architectures represent the number of neuronsin its corresponding layers.
Figure 18 presents correlation between predicted settle-ments versus calculated ones for the best network, 5-3-12-1.
Moreover, the predicted and calculated datasets areshown in Figure 19.
(2) Performance of Neural Networks in the Combined Static-Dynamic Loading Case. The results of evaluations of the
Applied Computational Intelligence and Soft Computing 19
Table 3: Performance of neural networks in the static case.
Network architecture RMSE 𝐴 𝑅25-5-1 0.2379 −0.025 0.1535-10-1 0.2371 0.032 0.1735-13-1 0.1275 0.024 0.1315-3-12-1 0.1829 0.967 0.895-5-10-1 0.2075 −0.006 0.221
0.2 0.4 0.6 0.8 10Measured
0
0.1
0.2
0.3
0.4
0.5
0.6
0.7
0.8
0.9
Pred
icte
d
y = 0.8945x + 0.0402
R2 = 0.9665
Figure 18: Correlation between predicted settlements versus calcu-lated ones for the best static neural network, 5-3-12-1.
Desired output and actual network output
Measured settlementPredicted settlement
0
0.1
0.2
0.3
0.4
0.5
0.6
0.7
0.8
0.9
1
Out
put
2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 221Exemplar
Figure 19: Predicted settlements versus calculated ones for the beststatic neural network, 5-3-12-1.
developed models in the coupled static-dynamic loadingcases are presented in Table 4.
Figure 20 presents correlation between predicted settle-ments versus calculated ones for the best network, 5-8-8-1.
0
0.1
0.2
0.3
0.4
0.5
0.6
0.7
0.8
0.9
1
Pred
icte
d
0.2 0.4 0.6 0.8 10Measured
y = 0.9826x + 0.0122
R2 = 0.9704
Figure 20: Correlation between predicted settlements versus calcu-lated ones for the best static- dynamic neural network, 5-8-8-1.
Moreover, the predicted and calculated datasets areshown in Figure 21.
6.2. EPR Models. Using EPR modeling, different relationshave been developed for both static and coupled static-dynamic settlements based on input parameters. Equations(10) show the best optimum relations for settlement predic-tion in static and coupled static-dynamic loading conditions,respectively.
𝑆𝑠 = −0.46228 (𝑝0.5) ln [( 𝑙𝑑) + 1]0.5 ln (𝑝 + 1)+ 0.1153 (𝑝) ln [( 𝑠𝑑) + 1]0.5
+ 0.0034446 (𝑝2) + 0.12898 (𝑁𝑝) (𝑑0.5)+ 26.5835,
(10)
𝑆csd = 0.16409 (𝑝) ( 𝑙𝑑) sech( 𝑙𝑑)0.5
+ 9.1863 (𝑑0.5) (𝑝0.5) sech( 𝑠𝑑)+ 0.97359𝑁𝑝0.5 + 1.7638,
(11)
20 Applied Computational Intelligence and Soft Computing
Table 4: Performance of neural networks in the coupled static-dynamic loading case.
Network architecture RMSE 𝐴 𝑅25-5-1 0.2508 0.016 0.2715-10-1 0.298 −0.016 0.2515-13-1 0.2441 0.026 0.225-3-12-1 0.3391 −0.001 0.2585-5-10-1 0.3115 −0.004 0.8245-8-8-1 0.039 0.983 0.97
Desired output and actual network output
Normalized settlementPredicted settlement
0
0.1
0.2
0.3
0.4
0.5
0.6
0.7
0.8
0.9
1
Out
put
2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 221Exemplar
Figure 21: Predicted settlements versus calculated ones for the beststatic-dynamic neural network, 5-8-8-1.
where 𝑆𝑠, 𝑆csd, 𝑝, 𝑙, 𝑑, 𝑠, and 𝑁𝑝, respectively, represent staticsettlement, coupled static-dynamic settlement, axial staticload, pile length, pile diameter, spacing, pile radius, andnumber of piles. Also, sech(𝑥) is the hyperbolic secant of (𝑥).
As it is shown in Figures 22 and 23, the coefficients ofdetermination for both static and static-dynamic coupledmodels presented using EPR are acceptable values of 97.49%and 97.26%, respectively, which mean that the proposedmodels are capable for predicting the settlements based onthe studied input parameters. Moreover, the values of RMSEfor static and coupled static-dynamic settlement models are0.271 and 0.364, respectively.
6.3. Sensitivity Analysis. Thestrength of relationship betweenaffecting parameters (number of piles, radius, ratio of 𝑠/𝑑,ratio of 𝑙/𝑑, and axial force) and the values of settlements ofCPRF in both static and coupled static-dynamic conditionscan be found using sensitivity analysis based on CosineAmplitude Method (CAM) [33] of CPRF in both static andcoupled static-dynamic conditions.
0
2
4
6
8
10
12
2 4 6 8 10 120
y = 0.9749x + 0.1496R2 = 0.9749
Calculated “Ss”
EPR
pred
ictio
n fo
r “S s
”
Figure 22: The calculated values of static settlement versus itscorresponding EPR prediction.
2 4 6 8 10 12 1400
2
4
6
8
10
12
14
EPR
pred
ictio
n fo
r the
settl
emen
ts
y = 0.9726x + 0.1829
R2 = 0.9726
Calculated “S=M>”
Figure 23: The calculated values of coupled static-dynamic settle-ments versus its corresponding EPR prediction.
In this method, the strength of relationship betweentarget parameter and inputs is found using [33, 41]:
𝑟𝑖𝑗 = ∑𝑘𝑚=1 𝑥𝑖𝑚𝑥𝑗𝑚√∑𝑘𝑚=1 𝑥2𝑖𝑚∑𝑘𝑚=1 𝑥2𝑗𝑚
, (12)
where each of the input parameters is expressed as one of 𝑋array’s elements shown in [33]
𝑋 = {𝑥1, 𝑥1, . . . , 𝑥𝑖, . . . , 𝑥𝑛} , (13)
Applied Computational Intelligence and Soft Computing 21
92.693.9 93.7
88.4
97.3
Number of piles r (m) s/d l/d P (kPa)Stre
ngth
of r
elatio
nshi
p be
twee
n co
ncer
ning
pa
ram
eter
s and
stat
ic se
ttlem
ents
of C
PRF
(%)
82
84
86
88
90
92
94
96
98
Figure 24: Strength of relationship between input parameters andCPRF settlements in the static case.
91.192.5 92.2
86.2
96.1
Number of piles r (m) s/d l/d P (kPa)
Stre
ngth
of r
elat
ions
hip
betw
een
conc
erni
ng p
aram
eter
san
d co
uple
d sta
tic-d
ynam
ic se
ttlem
ents
of C
PRF
(%)
80828486889092949698
Figure 25: Strength of relationship between input parameters andCPRF settlements in the coupled static-dynamic case.
where each of its elements is a vector with the length of 𝑘 andis presented in [33]
𝑥𝑖 = {𝑥𝑖1, 𝑥𝑖2, 𝑥𝑖3, . . . 𝑥𝑖𝑘} . (14)
Figures 24 and 25 show the strength of relationship betweeninput parameters and CPRF settlements in static and coupledstatic-dynamic case, respectively. As it can be seen, axial loadis the most important parameter in both conditions. Also,𝑙/𝑑 is the least effective parameter on the static and coupledstatic-dynamic CPRF’s settlements. Besides, effects of otherconcerning parameters on the settlements are quiet the same.
7. Conclusion
Knowing the piled raft settlements in static and coupledstatic-dynamic loading conditions plays an important rolein preliminary design phase of these combined foundations.Regarding the high expenses of full-scale model tests andexperimental tests in determining the earthquake inducedsettlements of the combined piled raft foundation and, also,
crucial need for quite a speedy and inexpensive predictivemethod, the applicability of neural network modeling hasbeen investigated and compared. Moreover, the large calcu-lation times available in commercial finite element or finitedifference software programs for dynamic complicated prob-lems makes the problem time-consuming. Hence, a speedyand accurate tool for predicting these values will significantlyhelp the engineers to facilitate the design procedure. In thisregard, the highly in-demand predictive tools, ANN, and EPRmodeling have been considered to forecast the settlements inboth static and coupled dynamic-static loading conditions.In this regard, dynamic nonlinear finite difference modelinghas been used to prepare the required datasets. After well-validating the used numerical procedure and applying a para-metric study, a databank consisting of 144 datasets has beengained. Using the developed databank, different ANNs andpolynomial regression models have been constructed, whichcan be efficiently used to predict the values of settlements forall the cases that there are similar available input parameters.Moreover, using the sensitivity analysis, themost and the leasteffective parameters on the static and coupled static-dynamicsettlements have been determined. Based on the obtainedresults, the following can be concluded:
(i) Neural networks are introduced as capable effectivetools for predicting static and coupled static-dynamicsettlements of CPRFs.
(ii) The best neural network in static case is 5-3-12-1 FFBPneural network with RMSE of 0.1829, 𝑅2 of 0.967, and𝐴 of 0.89.
(iii) In the case of coupled static-dynamic loads, thenetwork with the architecture of 5-8-8-1, RMSE of0.039, 𝑅2 of 0.97, and 𝐴 of 0.983 is the best obtainedneural network.
(iv) Based on EPR modeling, a new relationship withcoefficient of determination of 97.49% and RMSE of0.271 and the line slope of 0.975 for predicting thestatic settlements of combined piled raft foundationshas been proposed.
(v) A new relationship with coefficient of determinationof 97.26% and RMSE of 0.137 and the line slopeof 0.973 for predicting the coupled static-dynamicsettlements of combined piled raft foundations hasbeen presented.
(vi) Sensitivity analysis emphasized that axial load playsan important role in calculating static/coupled static-dynamic settlements and neglecting its effects willlead to significant errors in calculations. It was alsoshown that the effect of 𝑙/𝑑 on the settlements is lessthan other concerning parameters.
Based on the results, some efficient and highly capable toolsfor predicting static and coupled static-dynamic settlementsof CPRFs are suggested, which can be successfully used topredict the values of settlements in preliminary step of CPRFdesign.
22 Applied Computational Intelligence and Soft Computing
Conflicts of Interest
The authors declare that they have no conflicts of interest.
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