Published: 06 February 2021

Applying deep learning and wavelet transform for predicting the vibration behavior in variable thickness skew composite plates with intermediate elastic support

Wael A. Altabey1
1International Institute for Urban Systems Engineering (IIUSE), Southeast Universi, Nanjing, 210096, Jiangsu, China
1Department of Mechanical Engineering, Faculty of Engineering, Alexandria University, Alexandria, 21544, Egypt
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Abstract

In this paper, the vibration behavior features are extracted from the combination between Wavelet Transform (WT), and Finite Strip Transition Matrix (FSTM) of skew composite plates (SCPs), with variable thickness, and intermediate elastic support. Although, the results of this technique and based on the previous work done by the authors, that show the method can reflect the vibration behavior of the composite plates. Due to the method's difficulty in terms of, a lot of calculations with a large number of iterations these results may not be good choices for quick and accurate vibration behavior extracting. Thus, the new deep neural network (NN) is designed to learn and test these results carrying out by extracting vibration behavior features that reflect the important and essential information about the mode shapes in SCP. The results give high indications about the proposed technique of deep learning is a promising method, particularly when the type structures are complicated and the ambient environment is variable.

Applying deep learning and wavelet transform for predicting the vibration behavior in variable thickness skew composite plates with intermediate elastic support

Highlights

  • Extract the vibration behavior features of skew composite plates, with variable thickness, and intermediate elastic support from the combination between wavelet transform, and finite strip transition matrix.
  • Design the new deep neural network to learn and test these results carrying out by extracting vibration behavior features that reflect the important and essential information about the mode shapes in skew composite plate.
  • The results give high indications about the proposed technique of deep learning is a promising method, particularly when the type structures are complicated and the ambient environment is variable.

1. Introduction

The importance of to use of composite materials in many fields of technology, such as aerospace industries, marine engineering, and civil engineering is due to special features, e.g. high strength/weight ratio and corrosion resistance property, particularly under the effects of the harsh environment. Although the structures are made of these types of materials have some drawback are subject to matrix cracks, fiber breakage, and delamination. These invisible faults can lead to catastrophic structural failures [1-4].

Other major modes of failure of fiber-reinforced polymer (FRP) have a temperature, bending, tensile, stress, impact failure, and failure of the installation, etc. These types of failures are complicated and are not easy to assets, mostly when subjected to associate effects of multiple factors [5-7].

The user of an active system of structural health monitoring (SHM) to observe the safety and potential damage detection in composite plates are essential and most seriously. The function of SHM is consists of three main sub-functions, including system identification, features extraction for algorithms for detection and prediction, and reliability and risk evaluation [8-19].

The vibration behavior of composite structures is the traditional method for the intelligent detecting the defects in the composite. The mode shapes of the structure are one of the essential tools in Structural health monitoring (SHM) in the last decades, where, extracted the vibration response of composite structure for each damage type and position and analysis based on the variance in vibration parameters. In recent years, different techniques to extract the natural frequencies of composite plates have become a field of great interest in the scientific society [20-34].

To find the mode shapes for different boundary conditions with IES, numerical methods or experimental methods must be used. Some researchers have been interested in the vibration of multi-span plates using different approaches. In previous works, Altabey [35, 36] used the FSTM as one of the common use of semi-analytical approaches to extract vibration response of basalt FRP laminated variable thickness rectangular plates with IES, and he tried to improve the results accuracy and by the way, decrease the calculations efforts due to a large number of iterations by combined his method with artificial neural networks (ANNs) and response surface (RS) methods.

In the present research, the new deep NN is designed to predict the vibration behavior of SCPs with variable thickness and IES with a different elastic restraint coefficient (KT) and four cases of boundary conditions (BCs) of plate edges, namely SSSS, CCCC, SSFF, and CCFF. The plate is a rectangular SCP with variable thickness function h(y), the locations of the IES is at mid-line of the presented plate, and the plate was manufactured from basalt fiber reinforced polymer (BFRP) by using five symmetrically layers with the stacking angle [45°/–45°/45°/–45°/45°] as shown in Fig. 1. First, review the illustrated results of the utilized method by the combination of these WT and FSTM methods (WT-FSTM) to convergence the studies by checking the agreement with the results available in the literature. Second, the trained deep NN is used to predict the outcome of the extracted vibration behavior of SCPs from WT-FSTM at certain values of elastic restraint coefficients (KT) for IES, and then it is subsequently used to predict the vibration behavior for different levels of elastic restraint coefficients (KT) for IES. The results are predicted from the deep NN model are in very good agreement with the WT-FSTM results. Hence, the results give high indications about the proposed technique of deep learning is a promising method.

Fig. 1The geometry of rectangular SCP with variable thickness and IES

The geometry of rectangular SCP with variable thickness and IES

2. Model overview

The composite plate material has corresponding elastic and shear modulus values are shown in Table 1.

Table 1Model property

E11 (GPa)
E22 (GPa)
υ12
υ21
G12(GPa)
G21 (GPa)
rho kg/m3
96.74
22.55
0.3
0.6
10.64
8.73
2700

The normalized partial differential equation of vibration behavior for the plates system illustrated in Fig.1 under the assumption of the classical deformation theory in terms of the plate deflection wox,y,t using the non-Dimensional variables ξ and η related to the skew coordinate system u,ν,ϕ defined by u=xsecϕ, ν=y-xtanϕ, and ξ=ua, η=νb, and after some derivation, the governing equation can be written as follows:

1
ψ1h3(η)1a4Wξξξξ-4βsinϕψ3h3(η)Wξξξη+νβ2ψ2cos2ϕ2h3(η)η2Wξξ
+2β2ψ2cos2ϕh3(η)ηWξξη+2β2ψ2h3(η)3sin2ϕ+cos2ϕWξξηη
+2β4cos2ϕh3(η)ηWηηη-2β3ψ4νsinϕcos2ϕ2h3(η)η2Wξη
-4β3ψ4sinϕh3(η)Wξηηη+β4νtan2ϕ+1cos4ϕ2h3(η)η2Wηη
+β4h3ηWηηηη-4β3ψ4sinϕcos2ϕh3ηηWξηη=-Ω2hηho2cos4ϕWtt,

where ψ1=D11D22, ψ2=(D12+2D66)D22, ψ3=D16D22, ψ4=D26D22.

Since the treatment of IES conditions are the main objective of this paper we presented it in more detail. The line of the IES y=b/2, the displacement must vanish and the normal moment must be continuous, i.e.

2
KTwo=-2ψ33wox3-3woy3-ψ52wox2y-4ψ43woxy2,
3
woy η=1-/2=woy η=1+/2,

where: ψ1=D11D22, ψ2=(D12+2D66)D22, ψ3=D16D22, ψ4=D26D22, KT=Tb/2b3D22, ψ5=(D12+4D66)D22.

3. Determination of vibration behavior using WT and FSTM

In This section, the mode shapes of the SCP will be extracted using a new method by combined between the WT and FSTM methods with an adjusting frequency parameter, in order to improve the estimated accuracy of extracting by optimized the WT entropy for adjusting frequency parameter.

3.1. Continuous wavelet transform (CWT)

Continuous wavelet transform (CWT) is a convolution process of the data sequence with a set of continuous scaled and translated versions of the mother wavelet (MW) ψt. The translating process is a smoothing effect over the length of the data sequence to localize the wavelet in time domain x(t), whereas the scaling process is compressing or stretching of analyzed wavelet which indicates various resolutions. The stretched wavelet is used to capture the slow changes; while the compressed wavelet is used to capture abrupt changes in the signal. The trade-off of enhancing resolution is between increased computational cost and memory by computing wavelet components and multiplying each component by the correctly dilated and translated wavelet, resulting in the constituent wavelet of the analyzed signal [37-45].

The ψt is stretched or squeezed through varying its dilation parameter s and moved through its translation parameter τ (i.e. along the localized time index τ):

4
ψs,τ t=1 sψt-τs, τR, S>0.

Let x(t) be the system shape function response of FSTM, where t denotes time. CWT of a function x(t) L2(R), where L2(R) is the set of square-integrable functions is denoted as Ws,τ and defined as:

5
Ws,τ =xt,ψs,τ t= 1s-xt.ψ*t-τsdt,

where the wavelet scale s and the period τ are used to adjust the frequency and time location. Ws,τ shows how closely ψs,τ t correlated with x (t). By inverse CWT, the signal x(t) can be regenerated as:

6
xt=1Cψ -+-+Ws,τ ψs,τ dsdτS2.

For a plate striped in the ξ-direction by divided into N discrete longitudinal strips spanning between supports as shown in Fig. 1, the free-response equation for one striped beam system may be assumed in the form:

7
xt=XiξYiηejωτ.

The WT of Eq. (7) is:

8
Ws0,τ =s02XiξYiη.ψ*S0ωejωτ.

The logarithm of Eq. (8) gives:

9
lnWs0,τ =jωτ+lns02XiξYi(η)ψ*S0ω.

By using the straight line of the slope of the logarithm of WT modulus, we can be obtained the natural frequency of the system and it is given by:

10
ArgWs0,τ=ωτ ddτ ArgWs0,τ=ω.

The plot of ddτ Arg Ws0,τ is constant in the time domain and is equal to the natural frequency ω. The non-dimensional frequency parameter (NDFP) (Ω) are addressed in the form:

11
Ω=mohηω2a4hoD2212.

4. Deep neural networks (NNs)

Recently, deep learning, which is a network with multiple hidden layers of neurons, has also been applied in solving and identifying the ordinary and partial differential equations [46, 47].

Deep neural networks (NNs) are one of the artificial intelligence (AI) algorithms used for solving advanced non-linear problems [48]. The networks are consist of computational nodes that connected together to create one individual network, each node is processing a calculation on input and sends the result to output connections, and maybe a node output is an input to one other node or more.

In this section, we use the outcome of the results in Section 3 of vibration behavior of SCP extracted by WT-FSTM at certain values of elastic restraint coefficients (KT) to obtain the training data and to predict the vibration behavior for different levels of elastic restraint coefficients (KT) not included in the results.

The proposed deep NN architecture connection is presented in Fig. 2. The steps of the NDFP (Ω) prediction can be described through the following steps in Table 2.

Fig. 2The architecture of the proposed deep NN for the NDFP (Ω) prediction

The architecture of the proposed deep NN for the NDFP (Ω) prediction

Table 2The steps of deep NN training to predict NDFP (Ω)

NN steps
Step remark
Data collecting
Extract the training data from the WT-FSTM of the SCP at certain values of elastic restraint coefficients (KT)
Training model
Divide the extracting data into three groups of data, the first one will be used for training in MS-NN for mode shapes λi prediction of SCP, and the second group of a dataset will be used for training in W-NN for predicting deflection wox,t, this network without hidden layers
Testing model
The last part of the data will use to test the trained model in the training model. If the model is well-trained, the predicted results by the W-NN and MS-NN will be convergence to the real value. The training performance of suggested Deep NN is presented in Fig. 3
Prediction response
The response MS-NN will be used to predict the λi under random deflection wox,t. W-NN will be used to predict the wox,t at any location coordinate x along with the SCP including the IES location presented in Section 2

It is important for the NN designer to check his proposed deep NN performance is suitable or not from the formula of mean square error (MSE):

12
MSE=ΩNN-Ω2n.

Therefore, only one global minimum for performance index based on the features of the input vectors, but the minimum local minimum of a function at finite input values, and it cannot be omitted when attaching deep NN. Therefore, we can judge on accuracy a local minimum, if it has a low closer range to global minimum and low MSE. Anyway, the designer must be selected as a suitable method to solve this problem in order to descent the local minimum with momentum. Momentum allows a network to respond not only to the local gradient but also to recent trends in the error surface. Without momentum, a network may get stuck in a shallow local minimum. Fig. 3 shows the performance curves of training with three groups for learning data.

Fig. 3Training performance of proposed NN

Training performance of proposed NN

5. Results and discussion

In this section, after reviewing the results available in the literature, the approach of WT-FSTM are used to extract the vibration behavior of SCP with variable thickness are presented in Section 2 at certain values of elastic restraint coefficients (KT) for IES, on the other hand, to provide the active training data to proposed deep NN, in order to extract the influence of the IES on the natural frequencies with different elastic restraint coefficients (KT) of such plates.

5.1. Convergence study and accuracy

The importance for review of presented work results with the results available in the literature in order to validate the accuracy and reliability of the proposed technique. In this subsection, the WT-FSTM technique has been applied on a CCCC variable thickness SP with β=0.5,Δ= (0, 0.2, 0.4, 0.5) and ϕ= (30°, 45°, 60°), and then the convergence between the results in Fig. 4 with the results from FSTM [35] will be done.

As shown in the Fig. 4, after convergence, we can see clearly generally, that the results of the presented method WT-FSTM in excellent agreement with the other accurate methods in references [23-26, 35]. On the other hand, we can see the effects of plate Skew angles (ϕ), tapered ratio (Δ) and aspect ratio (β) on the NDFP (Ω) it has been increased with increasing of the ϕ, β, and Ω, in all methods WT-FSTM and the methods in the literature.

5.2. Proposed method (WT-FSTM) results

In the present study, the numerical computations using the WT-FSTM approach is applied to extract vibration behavior. Due to the method difficulty in terms of, a lot of calculations with a large number of iterations these results may not be good choices for quickly and accurate vibration behavior extracting, the new deep NN is designed to learn and test these results carrying out by extracting vibration behavior features that reflect the important and essential information about the mode shapes in SCP. The proposed method target achieved using only two different KT in computations of the NDFP (Ω), the first one is located at KT= 50 the second is KT= 750, respectively. The first six frequencies are presented in Table 3, the NDFP Ω has been computed with different values of skew angle (ϕ) at aspect ratio (β= 0.5), and tapered ratio (Δ= 0.5) to study the behavior of natural frequencies under a different skew angle for different four BCs namely SSSS, CCCC, SSFF, and CCFF.

Fig. 4Comparison of the first four natural frequencies of CCCC skew plates β= 0.5

Comparison of the first four natural frequencies of CCCC skew plates β= 0.5

Figs. (5-6) represent the comparison between the WT-FSTM data and the deep NN predicted data NDFP Ω for KT= 50 and KT= 750 respectively of four different BCs are SSSS, CCCC, SSFF, and CCFF. The results of the proposed deep NN show much satisfactory prediction quality for this case study.

Fig. 5Comparison between the WT-FSTM data and deep NN predicted data for KT= 50

Comparison between the WT-FSTM data and deep NN predicted data for KT= 50

a)ϕ=

Comparison between the WT-FSTM data and deep NN predicted data for KT= 50

b)ϕ= 30°

Comparison between the WT-FSTM data and deep NN predicted data for KT= 50

c)ϕ= 45°

Comparison between the WT-FSTM data and deep NN predicted data for KT= 50

d)ϕ= 60°

Fig. 6Comparison between the WT-FSTM data and deep NN predicted data for KT= 750

Comparison between the WT-FSTM data and deep NN predicted data for KT= 750

a)ϕ=

Comparison between the WT-FSTM data and deep NN predicted data for KT= 750

b)ϕ= 30°

Comparison between the WT-FSTM data and deep NN predicted data for KT= 750

c)ϕ= 45°

Comparison between the WT-FSTM data and deep NN predicted data for KT= 750

d)ϕ= 60°

Table 3The first six frequencies of SCP, β= 0.5, Δ= 0.5

BCs
ϕ
KT
Ω1
Ω2
Ω3
Ω4
Ω5
Ω6
SSSS
50
22.157
36.232
53.594
78.249
105.594
138.710
750
55.078
69.159
86.525
111.179
138.523
171.633
30°
50
39.507
49.713
69.226
98.139
135.487
179.658
750
72.428
82.640
99.1570
131.069
166.416
212.581
45°
50
57.936
69.256
87.408
119.321
156.736
201.733
750
90.857
102.183
120.339
152.251
194.665
234.656
60°
50
112.564
127.407
148.221
177.583
204.928
238.044
750
145.485
160.334
181.152
210.513
237.857
270.967
CCCC
50
28.446
46.511
68.806
100.457
135.565
178.079
750
61.361
79.435
101.737
133.372
168.490
211.102
30°
50
45.796
59.992
85.438
120.347
166.458
219.027
750
78.711
92.916
114.369
153.262
196.383
252.050
45°
50
64.225
79.535
102.620
141.529
191.707
241.102
750
97.140
112.459
135.551
174.444
224.632
274.125
60°
50
118.853
137.686
163.433
199.791
234.899
277.413
750
151.768
170.610
196.364
232.706
267.824
310.436
SSFF
50
12.286
20.083
29.716
43.375
58.538
76.887
750
45.206
53.013
62.639
76.305
91.465
109.813
30°
50
31.636
36.564
48.348
66.265
90.431
117.835
750
62.556
66.494
75.271
96.195
119.358
150.761
45°
50
48.065
53.107
63.530
84.447
110.680
139.910
750
80.985
86.037
96.453
117.377
143.607
172.836
60°
50
102.693
111.258
124.343
140.709
157.872
176.221
750
135.613
144.188
157.266
173.639
190.799
209.147
CCFF
50
19.603
32.054
47.423
69.228
93.425
122.724
750
52.529
64.981
80.346
102.154
126.355
155.641
30°
50
36.953
47.535
64.055
91.118
126.318
163.672
750
69.879
78.462
92.978
122.044
154.248
196.589
45°
50
55.382
65.078
81.237
110.300
149.567
185.747
750
88.308
98.005
114.160
143.226
182.497
218.664
60°
50
110.010
123.229
142.050
168.562
192.759
222.058
750
142.936
156.156
174.973
201.488
225.689
254.975

5.3. Deep NN performance

The performances of suggested deep NN are presented in Table 4 and Fig. 3, the MSE and accuracy of predicted data are calculated from Eq. 12 for NDFP (Ω). From Table 4 and Fig. 3 the value of MSE and accuracy of training data are 7.2 E-5 and 99.7 % respectively and validating data are 6.2 E-5 and 99.8 % respectively. From NN performance shows in Table 4 and Fig. 3, the proposed deep NN gave a good prediction for vibration behavior data in the presented SCP.

Table 4Mean square error (MSE) and accuracy values

Data
MSE
Accuracy
Training
7.2 E-5
99.7 %
Validating
6.2 E-5
99.8 %

5.4. Deep NN predicting results

In this subsection, the main target of design the deep NN of predicting the vibration behavior data of SCP under different elastic restraint coefficients (KT) is achieved, chosen 7 different KT for different four BCs (SSSS, CCCC, SSFF, and CCFF). The deep NN predicted results of the first six frequencies of SCP with β= 0.5 and Δ= 0.5 are shows in Fig. 7.

Moreover, the influence of the IES on the vibration behavior of the SCPs with variable thickness is shown in Fig. 7. As shown in the Fig. 7 for all values of skew angle (ϕ) and all types of BCs, the first six frequencies are increasing with increasing of the value of elastic restraint coefficient (KT). whereas the frequencies rapidly increase with for small values of elastic restraint coefficient (KT), and the influence of IES becomes negligible at high values. On the other hand for all values of skew angle (ϕ), the first six frequencies for fully clamped (CCCC) plate are the highest frequencies, and the semi-simply supported (SSFF) plate is the lowest one, while, the other two boundaries (SSSS and CCFF) were rested between them. also, we can see the effects of plate skew angles (ϕ) on the NDFP (Ω) it has been increased with increasing of the. skew angles.

Fig. 7The deep NN predicted results of NDFP (Ω)

The deep NN predicted results of NDFP (Ω)

a) SSSS

The deep NN predicted results of NDFP (Ω)

b) CCCC

The deep NN predicted results of NDFP (Ω)

c) SSFF

The deep NN predicted results of NDFP (Ω)

d) CCFF

6. Conclusions

By a combination of the WT and FSTM method (WT-FSTM) was used to extract the vibration behavior of SCP with variable thickness, and IES, the plate is made from BFRP laminated. First, To investigate from accuracy and reliability of the proposed technique, the convergence between the proposed study results with the results available in the literature has been checked, thus validating the accuracy and reliability of the proposed technique. Then, due to the proposed method's difficulty in terms of, a lot of calculations with a large number of iterations, these results may not be good choices for quick and accurate vibration behavior extracting. Thus, the new deep neural network (NN) is designed to learn and test these results carrying out by extracting vibration behavior features that reflect the important and essential information about the mode shapes in SCP. The influence of β, Δ, ϕ, and KT on the predicted NDFP (Ω) of the plate, has been studied, with four different support conditions (SSSS, CCCC, SSFF, and CCFF).

Based on the WT-FSTM and the deep NN predicted results, we conclude that the deep NN predicted results of NDFP (Ω) are in very good agreement with the proposed method results WT-FSTM with an accuracy of training and validating data are 99.7 % and 99.8 % respectively.

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About this article

Received
18 May 2020
Accepted
30 December 2020
Published
06 February 2021
SUBJECTS
Mechanical vibrations and applications
Keywords
free vibration
deep learning
wavelet transform (WT)
variable thickness plates
skew composite plates (SCPs)
BFRP