Document Type : Research Article
Author
Department of Mathematics, Government Girls Degree College, Behat- 247121, India
Abstract
Keywords
Main Subjects
Effect of Elastically Restrained Edges on Free Transverse Vibration of Functionally Graded Porous Rectangular Plate
Department of Mathematics, Government Girls Degree College, Behat- 247121, India
KEYWORDS |
|
ABSTRACT |
Functionally graded; Porous rectangular; Restrained; Physical neutral surface; Rayleigh-Ritz. |
In this paper, the author studied free transverse vibration of a thin isotropic simply-supported functionally graded (FG) rectangular plate with porosity effect based on classical plate theory. The plate is considered to be elastically restrained against rotation. It is assumed that the material properties of the graded plate are porosity-dependent. An even porosity distribution is considered for analysis purposes. Due to the asymmetry of material in the thickness direction, the neutral surface is not the same as the geometrical mid-plane of the plate. The concept of the physical neutral surface of the FG plate along with classical plate theory is used to formulate the problem. Hence, the physical neutral surface is taken as the reference plane. The first three dimensionless frequencies of the plate are obtained using the Rayleigh-Ritz method. Boundary characteristic orthogonal polynomials (eigenfunctions), generated using the Gram-Schmidt process, are used in the Rayleigh-Ritz method. A parametric study shows that porosity and material distribution parameters have remarkable effects on the free vibration response of the plate. Results are compared with those of simply-supported FG plates. |
Functionally graded materials, generally made of ceramic and metal, are nonhomogeneous materials in which material properties vary continuously in appropriate directions. Free transverse vibration analysis of FG rectangular plates has gained attention of many researchers. A few papers about free vibration of FG plates have appeared in the literature and are summarized as follows: Dynamic response of initially stressed FG rectangular thin plates resting on elastic foundation has been studied by Yang and Shen [1]. Abrate [2] studied free vibrations, buckling, and static deflections of FG rectangular plates. He concluded that the natural frequencies of FG plates are proportional to those of homogeneous isotropic plates. Ferreira et. al. [3] computed natural frequencies of square FG plates employing the asymmetric collocation method. Zhao et. al. [4] presented the mechanical and thermal buckling analysis of FG rectangular plates using first-order shear deformation theory and the element-free kp-Ritz method. Talha and Singh [5] studied static and free vibration of FGM plates using higher order shear deformation theory in conjunction with FEM. Janghorban and Zareb [6] investigated the thermal effect on free vibration of FG arbitrary straight-sided plates with circular and non-circular cut-outs. Ghannadpour et. al. [7] used the finite strip method to analyse the buckling behaviour of FG rectangular plates under thermal loading. The plates were subjected to distributed impulsive loads. Thermal buckling of FG skew and trapezoidal plates has been investigated by Jaberzadeh et. al. [8] using the element-free Galerkin method. Baferani et. al. [9] investigated free vibration of FG rectangular plates based on first-order shear deformation theory. Chakraverty and Pradhan [10-11] investigated free vibration of thin FG rectangular plates incorporating the effects of Winkler foundation and thermal environment using the Rayleigh-Ritz method. Pradhan and Chakraverty [12] dealt with static analysis of thin FG rectangular plates under mechanical load using the Rayleigh-Ritz method. Khorshidi and Bakhsheshy [13] investigated the vibration analysis of FG rectangular plates partially in contact with a fluid. Pham [14] developed an analytical solution to investigate the thermal buckling of imperfect rectangular plates with FG coating under uniform temperature rise. Atmane et. al. [15] studied thermal buckling of a simply supported sigmoid FG rectangular plate employing first-order shear deformation theory. Lee et. al. [16] presented a thermal buckling analysis of FG rectangular plates based on the neutral surface of a structure. Kumar et. al. [17] investigated free vibration of thin FG rectangular plates using the dynamic stiffness method.
The materials having pores are termed as porous materials. The application of these materials in the aeronautical industry, energy absorbing systems, sound absorbers, insulating materials, heat exchangers, construction materials, and electromagnetic shielding has necessitated the study of different behaviors of structures made of porous materials in recent years [18]. A significant number of works dealing with the static, bending, vibration, and buckling problems of porous beams and plates are reviewed as follows: Theodorakopoulos and Beskos [19] studied flexural vibration of thin, rectangular, simply-supported, and fluid-saturated porous plates. Leclaire et. al. [20] presented a simple model of the transverse vibration of a thin rectangular porous plate saturated by a fluid. The vibration of a clamped rectangular porous plate using Galerkin’s variational method has been presented by Leclaire et. al. [21]. Vibration analysis of porous FG beams was presented by Wattanasakulpong and Ungbhakorn [22]. Razaei and Saidi [23] presented an exact solution for the vibration of rectangular porous plates using Reddy’s third-order shear deformation theory. Mojahedin et. al. [24] studied the buckling of FG circular porous plates using the energy method based on higher-order shear deformation theory. Chen et. al. [25] presented free and forced vibration of FG porous beams with different kinds of porosity distributions. Ebrahimi and Habibi [26] presented a finite element formulation for deflection and vibration of FG porous plates based on higher-order shear deformation theory. Mechab et. al. [27-28] studied free vibration/probabilistic analysis of FG nanoplate with porosities resting on Winkler-Pasternak elastic foundation. Jahwari and Naguib [29] presented an analysis of FG viscoelastic porous structure with a higher order plate theory. Barati et. al. [30] used a refined four-variable theory to study the buckling of FG piezoelectric porous plates resting on an elastic foundation. Barati and Zenkour [31] explored the electro-thermo-mechanical vibrational behavior of FG piezoelectric plates with porosity using a refined four-variable plate theory. Mouaici et. al. [32] used hyperbolic shear deformation theory to examine the effect of porosity on the vibration of non-homogeneous plates. Ebrahimi and Jafari [33] presented an analytical solution to study the buckling characteristics of porous magneto-electro-elastic FG plates. In a series of papers, Rezaei and co-workers [34-40] studied the free vibration and buckling behavior of porous plates employing various plate models. Kamranfard et. al. [41] presented an analytical solution for vibration and buckling of porous annular sector plates under in-plane uniform compressive loads. Şimşek and Aydın [42] used a modified couple stress theory to study the forced vibration of FG microplates with porosity effects. Akbas [43] dealt with free vibration and static bending of simply supported FG plates with porosity effect incorporating first-order shear deformation theory. Barati and co-workers [44-47] have presented vibration analysis of smart/nano FG porous plates using a refined four-variable theory. Ali et. al. [48] studied free vibration of the embedded porous plate using higher order shear deformation theory. Wang and Zu [49-51] studied free/forced vibration of FG rectangular porous plates with different complicating effects. Wang and Yang [52] investigated the nonlinear vibration of moving FG plates in contact with liquid and containing porosities. Electro-mechanical vibration analysis of FG piezoelectric porous plates in the translation state has been presented by Wang [53]. Kiran et. al. [54] studied the effect of porosity on the structural behavior of skew functionally graded magneto-electro-elastic plates. Free vibration analysis of saturated porous circular plates made of FG material integrated with a piezoelectric actuator is presented by Arshid and Khorshidvand [55] using the differential quadrature method. Arani et. al. [56] dealt with the dynamic analysis of rectangular porous plates resting on the Pasternak foundation using high-order shear deformation theory. Gupta and Talha [57] presented the influence of porosity on flexural and free vibration of FG plates in a thermal environment based on non-polynomial higher-order shear and normal deformation theory. Zhao et. al. [58] studied free vibration of functionally graded porous rectangular plates by means of an improved Fourier series method considering three types of porosity distributions. Daikh and Zenkour [59] obtained a Navier solution of free vibration and mechanical buckling of porous functionally graded sandwich plates using higher-order shear deformation theory. Du et. al. [60] performed a free vibration analysis of rectangular plates with three types of porosity distributions using the Rayleigh-Ritz method based on first-order shear deformation theory. Rjoub and Alshatnawi [61] predicted the natural frequencies of a simply-supported functionally graded porous cracked plate using the Artificial Neural Network technique. Bansal et. al. [62] provided Navier solution and FEM-based solution of vibration of porous functionally graded plates with geometric discontinuities and partial supports based on the refined exponential shear deformation theory. Tran et. al. [63] presented static and free vibration of functionally graded porous plates using an edge-based smoothed finite element method. Chai and Wang [64] investigated traveling wave vibration of spinning graphene platelets reinforced porous joined conical-cylindrical shells using the power series method.
An up-to-date review of works pertaining to the application of the Rayleigh-Ritz method in vibration analysis of structural elements is given by Kumar [65] and Pablo et. al. [66]. In their two papers, Wang and co-workers [67-68] used the Rayleigh-Ritz method to analyze the vibration of longitudinally moving plate submerged in an infinite liquid domain and that of FG cylindrical shells with porosities.
In some engineering problems, the boundary conditions along the edges of the plate are assumed to be either clamped or simply supported. But the actual boundary conditions tend to be in between these two limiting cases. To achieve these boundary conditions, analysis is done by modeling the edge conditions as a collection of elastic springs whose combined effect could vary from zero to infinity. Very few researchers (Laura and Grossi [69], Okan [70], Kumar [71], Zhang et. al. [72], He et. al. [73]) have considered the effect of elastically restrained edges against rotation on the vibration of plates.
The objective of this work is to study the free transverse vibration of a thin isotropic FG rectangular plate with even porosity distribution. The plate is simply-supported and elastically restrained against rotation along the edges. Material properties of the plate, continuously varying in the thickness direction, are assumed to be dependent on porosity. The Rayleigh-Ritz method incorporating boundary characteristic orthogonal polynomials as eigenfunctions is used to obtain the first three natural frequencies and mode shapes.
Let us consider a thin isotropic FG elastically restrained against a rotation rectangular plate made of porous material with length ‘a’ taken in the x direction, breadth ‘b’ in the y direction and thickness ‘h’ in z direction as shown in Fig. 1. The top surface (h/2) is ceramic rich while bottom surface (-h/2) is metal rich.
The physical neutral surface does not coincide with the geometrical mid-plane of the plate. The distance between the geometrical mid-plane and the physical neutral surface is considered to be . There exists uniformly distributed (even) porosity in the plate. In this model, porosity spreads uniformly through the thickness direction.
The strains are defined as: |
|
|
(1) |
According to Hook’s law
|
(2) |
Using relation (1) in (2), we obtain
|
(3) |
The expression for the strain energy is
|
(4) |
Using relations (1) and (3) in (4), strain energy becomes
|
(5) |
Fig. 1. (i) FG porous elastically restrained rectangular plate with physical neutral surface and geometrical middle surface (ii) plate with even porosity (iii) cross-section of the plate
The kinetic energy of the plate is given as
|
(6) |
where is the displacement, is Young’s modulus, is the density, is the Poisson’s ratio, the subscript following a variable denotes differentiation of the variable w.r.to the subscript following it, and is the time.
The effective material properties viz. Young’s modulus and density are assumed to be graded in the thickness direction according to the power law (Wattanasakulpong and Ungbhakorn [22]) as follows:
|
(7) |
|
(8) |
where are young’s moduli of ceramic and metal; are densities of ceramic and metal; is the non-negative volume fraction index which describes the material distribution across the thickness of the plate and is porosity volume fraction. The value of equal to 0 corresponds to the perfect FG plate. The plate becomes isotropic homogeneous if either (fully ceramic) or (fully metal).
For harmonic solution, the displacement is assumed to be
|
(9) |
where is the circular frequency, represents the maximum transverse displacement at the point and .
Using relations (7), (8), and (9), the expressions for maximum strain energy and kinetic energy of the plate become
|
(10) |
and
|
(11) |
where
|
(12) |
|
(13) |
|
(14) |
|
(15) |
|
The maximum strain energy (Warburton and S.L. Edney [74]) associated with the rotational restraints in the edges is given by
|
(16) |
where are the rotational spring constants.
Introducing the non-dimensional variables together with
|
(17) |
We obtain the standard eigenvalue problem as follows:
|
(18) |
where is the order of approximation to get the desired accuracy, are orthonormal polynomials, are unknowns,
|
(19) |
|
|
|
|
, |
|
|
|
and is the frequency parameter.
The orthonormal polynomials are generated using the Gram-Schmidt process (Singh and Chakraverty [75]).
In this modal analysis, a plate made of functionally graded material (Aluminium/ Alumina, i.e., ) is considered. Here, the symbol is used for and represents The following values of material coefficients (Talha and Singh [5]) for the FG plate and other parameters are taken:
|
|
|
|
|
We also assume that the Poisson’s ratio remains constant along the thickness direction as the plate is considered to be thin. The first three values of the frequency parameter have been calculated from the standard eigenvalue problem given by (18). For this purpose, a computer program has been developed by the author in C++. Table 1 shows the convergence of frequency parameter with increasing . To achieve an accuracy of four decimal places, the value of has been fixed as 26. A comparison of frequencies of simply-supported isotropic FG rectangular/square plates is shown in Table 2. The results are in good agreement with those available in the literature. The results have been reported in Tables (3-5) and Figs. (2-7).
Table 1. Convergence of first three values of frequency parameter Ω of FG porous plate with increasing value of
|
|
|
|||||
|
Mode |
10 |
15 |
20 |
24 |
25 |
26 |
|
|||||||
0.3 |
I |
89.7801 |
10.2914 |
10.2914 |
10.2914 |
10.2914 |
10.2914 |
II |
179.1420 |
179.1420 |
21.2307 |
21.2264 |
21.2264 |
21.2264 |
|
III |
913.5480 |
179.1420 |
21.2390 |
21.2264 |
21.2264 |
21.2264 |
|
|
|||||||
0.3 |
I |
8923.51 |
10.2931 |
10.2931 |
10.2931 |
10.2931 |
10.2931 |
II |
17796.3 |
17796.3 |
21.2429 |
21.2429 |
21.2429 |
21.2429 |
|
III |
91336.8 |
17796.3 |
21.2430 |
21.2429 |
21.2429 |
21.2429 |
|
|
|||||||
0.1 |
I |
16078 |
64.7397 |
64.7397 |
64.7397 |
64.6713 |
64.6713 |
II |
30095.9 |
29615.5 |
83.7024 |
83.7024 |
83.7024 |
83.7024 |
|
III |
107816 |
30095.9 |
171.346 |
171.3450 |
119.9290 |
119.9290 |
|
|
|||||||
0.2 |
I |
29.5262 |
29.5218 |
29.5160 |
29.5160 |
29.5160 |
29.5160 |
II |
47.3251 |
47.3251 |
47.2301 |
47.2262 |
47.2262 |
47.2262 |
|
III |
99.1221 |
77.5665 |
77.5665 |
76.8723 |
76.7577 |
76.7577 |
|
|
|||||||
0.2 |
I |
15.2531 |
15.0241 |
15.0241 |
15.0238 |
15.0238 |
15.0238 |
II |
32.9505 |
32.9504 |
28.4808 |
28.4808 |
28.4808 |
28.4808 |
|
III |
36.5462 |
36.5462 |
35.9856 |
35.9856 |
35.9856 |
35.9856 |
Table 2. Comparison of frequency parameter Ω of simply-supported FG plate
|
|
Reference |
Mode I |
Mode II |
Mode III |
0 |
0.4 |
Leissa [76] |
11.4487 |
16.1862 |
24.0818 |
|
|
Present |
11.4487 |
16.1863 |
24.2984 |
|
1.0 |
Leissa [76] |
19.7392 |
49.3480 |
49.3480 |
|
|
Present |
19.7392 |
49.3490 |
49.3490 |
|
1.5 |
Leissa [76] |
32.0762 |
61.6850 |
98.6960 |
|
|
Present |
32.0762 |
61.6860 |
98.6982 |
0.2 |
1.0 |
Kumar et. al. [17] |
18.3177 |
45.7942 |
45.7942 |
|
|
Present |
18.3177 |
45.7951 |
45.7951 |
1.0 |
0.5 |
Kumar et. al. [17] |
9.4131 |
15.0610 |
24.4741 |
|
|
Present |
9.4131 |
15.0612 |
24.7371 |
|
1.0 |
Kumar et. al. [17] |
15.0610 |
37.6524 |
- |
|
|
Present |
15.0610 |
37.6531 |
- |
|
2.0 |
Kumar et. al. [17] |
37.652 |
60.244 |
97.896 |
|
|
Present |
37.6524 |
60.2447 |
97.9168 |
5.0 |
1.0 |
Kumar et. al. [17] |
12.9831 |
32.4578 |
32.4578 |
|
|
Present |
12.9831 |
32.4584 |
32.4584 |
Table 3. First three values of frequency parameter Ω of FG porous plate for
|
|
||||||
|
|
0 |
1 |
2 |
3 |
4 |
5 |
|
Mode |
|
|||||
0.0 |
I |
20.3576 |
16.7595 |
15.5579 |
15.1744 |
15.0228 |
14.9330 |
II |
28.1742 |
22.5141 |
20.7440 |
20.1829 |
19.9590 |
19.8262 |
|
III |
45.3146 |
37.7248 |
35.6836 |
35.1296 |
34.9489 |
34.8525 |
|
0.1 |
I |
20.8079 |
16.6007 |
14.9632 |
14.3858 |
14.1615 |
14.0502 |
II |
28.7066 |
22.1958 |
19.8414 |
19.0234 |
18.7051 |
18.5464 |
|
III |
46.2599 |
37.7577 |
35.1488 |
34.3706 |
34.1258 |
34.0306 |
|
0.2 |
I |
21.3262 |
16.2883 |
13.8835 |
12.8726 |
12.4421 |
12.2443 |
II |
29.3263 |
21.6684 |
18.2965 |
16.9092 |
16.3217 |
16.0518 |
|
III |
47.3702 |
37.6793 |
34.1196 |
32.8494 |
32.3928 |
31.9499 |
|
0.3 |
I |
21.9326 |
15.6980 |
11.6935 |
9.3033 |
7.8542 |
6.9551 |
II |
30.0596 |
20.7689 |
15.3005 |
12.1211 |
10.2133 |
9.0352 |
|
III |
48.6954 |
37.3800 |
30.5239 |
24.3207 |
20.5589 |
18.2235 |
|
|
|
||||||
0.0 |
I |
34.6795 |
26.9424 |
24.5964 |
23.8533 |
23.5532 |
23.3746 |
II |
70.9287 |
55.1290 |
50.3468 |
48.8330 |
48.2222 |
47.8587 |
|
III |
70.9287 |
55.1290 |
50.3468 |
48.8330 |
48.2222 |
47.8587 |
|
0.1 |
I |
35.2494 |
26.4107 |
23.3518 |
22.3010 |
21.8902 |
21.6839 |
II |
72.0935 |
54.0525 |
47.8166 |
45.6753 |
44.8387 |
44.4189 |
|
III |
72.0935 |
54.0525 |
47.8166 |
45.6753 |
44.8387 |
44.4189 |
|
0.2 |
I |
35.9161 |
25.6153 |
21.3390 |
19.6197 |
18.8964 |
18.5636 |
II |
73.4572 |
52.4395 |
43.7197 |
40.2136 |
38.7386 |
38.0605 |
|
III |
73.4572 |
52.4395 |
43.7197 |
40.2136 |
38.7386 |
38.0605 |
|
0.3 |
I |
36.7098 |
24.3647 |
17.6371 |
13.8647 |
11.6389 |
10.2761 |
II |
75.0818 |
49.8999 |
36.1736 |
28.4688 |
23.9184 |
21.1299 |
|
III |
75.0818 |
49.8999 |
36.1736 |
28.4688 |
23.9184 |
21.1299 |
|
|
|
||||||
0.0 |
I |
81.4036 |
67.0071 |
62.2002 |
60.6664 |
60.0599 |
59.7007 |
II |
112.6970 |
90.0566 |
82.9760 |
80.7316 |
79.8361 |
79.3049 |
|
III |
167.1160 |
130.9970 |
120.0990 |
116.6610 |
115.2840 |
114.4660 |
|
0.1 |
I |
83.2031 |
66.3703 |
59.8209 |
57.5116 |
56.6146 |
56.1699 |
II |
114.8260 |
88.7832 |
79.3657 |
76.0936 |
74.8202 |
74.1856 |
|
III |
169.9390 |
128.7410 |
114.4610 |
109.5510 |
107.6400 |
106.6850 |
|
0.2 |
I |
85.2746 |
65.1195 |
55.5028 |
51.4611 |
49.7399 |
48.9492 |
II |
117.3050 |
86.6735 |
73.1861 |
67.6369 |
65.2870 |
64.2072 |
|
III |
173.2520 |
125.2630 |
105.1450 |
96.9921 |
93.5559 |
91.9784 |
|
0.3 |
I |
87.6980 |
62.7578 |
46.7478 |
37.1944 |
31.4035 |
27.8106 |
II |
120.2380 |
83.0756 |
61.2021 |
48.4844 |
40.8531 |
36.1407 |
|
III |
177.2070 |
119.6390 |
87.5955 |
69.2985 |
58.3839 |
51.6567 |
Table 4. First three values of frequency parameter Ω of FG porous plate for
|
|
||||||
|
|
0 |
1 |
2 |
3 |
4 |
5 |
|
Mode |
|
|||||
0.0 |
I |
24.6096 |
18.7771 |
17.0717 |
16.5339 |
16.3162 |
16.1866 |
II |
31.8669 |
24.3144 |
22.1060 |
21.4097 |
21.1278 |
20.9599 |
|
III |
65.2334 |
49.7732 |
45.2527 |
43.8272 |
43.2501 |
42.9065 |
|
0.1 |
I |
24.9625 |
18.3586 |
16.1601 |
15.4106 |
15.1175 |
14.9701 |
II |
32.3237 |
23.7724 |
20.9256 |
19.9551 |
19.5756 |
19.3847 |
|
III |
66.1687 |
48.6639 |
42.8363 |
40.8496 |
40.0728 |
39.6820 |
|
0.2 |
I |
25.3817 |
17.7570 |
14.7195 |
13.5109 |
13.0037 |
12.7705 |
II |
32.8666 |
22.9934 |
19.0602 |
17.4952 |
16.8385 |
16.5364 |
|
III |
67.2800 |
47.0693 |
39.0177 |
35.8139 |
34.4697 |
33.8514 |
|
0.3 |
I |
25.8882 |
16.8410 |
12.1213 |
9.5079 |
7.9736 |
7.0364 |
II |
33.5225 |
21.8074 |
15.6958 |
12.3118 |
10.3250 |
9.1114 |
|
III |
68.6226 |
44.6413 |
32.1304 |
25.2031 |
21.1361 |
18.6517 |
|
|
|
||||||
0.0 |
I |
36.0000 |
27.4679 |
24.9732 |
24.1865 |
23.8680 |
23.6784 |
II |
74.2966 |
56.6881 |
51.5395 |
49.9160 |
49.2587 |
48.8673 |
|
III |
74.2966 |
56.6881 |
51.5395 |
49.9160 |
49.2587 |
48.8673 |
|
0.1 |
I |
36.5161 |
26.8557 |
23.6396 |
22.5432 |
22.1145 |
21.8989 |
II |
75.3618 |
55.4247 |
48.7874 |
46.5246 |
45.6399 |
45.1948 |
|
III |
75.3618 |
55.4247 |
48.7874 |
46.5246 |
45.6399 |
45.1948 |
|
0.2 |
I |
37.1294 |
25.9757 |
21.5323 |
19.7642 |
19.0224 |
18.6812 |
II |
76.6274 |
53.6085 |
44.4383 |
40.7894 |
39.2584 |
38.5541 |
|
III |
76.6274 |
53.6085 |
44.4383 |
40.7894 |
39.2584 |
38.5541 |
|
0.3 |
I |
37.8703 |
24.6357 |
17.7314 |
13.9085 |
11.6641 |
10.2931 |
II |
78.1565 |
50.8431 |
36.5941 |
28.7044 |
24.0724 |
21.2429 |
|
III |
78.1565 |
50.8431 |
36.5941 |
28.7044 |
24.0724 |
21.2429 |
|
|
|
||||||
0.0 |
I |
98.4856 |
75.1444 |
68.3194 |
66.1674 |
65.2961 |
64.7773 |
II |
127.4670 |
97.2574 |
88.4241 |
85.6387 |
84.5110 |
83.8396 |
|
III |
182.6360 |
139.3510 |
126.6940 |
122.7030 |
121.0870 |
120.1250 |
|
0.1 |
I |
99.8976 |
73.4696 |
64.6713 |
61.6719 |
60.4991 |
59.9091 |
II |
129.2950 |
95.0897 |
83.7024 |
79.8203 |
78.3024 |
77.5388 |
|
III |
185.2550 |
136.2450 |
119.9290 |
114.3660 |
112.1910 |
111.0970 |
|
0.2 |
I |
101.5750 |
71.0620 |
58.9063 |
54.0694 |
52.0399 |
51.1064 |
II |
131.4660 |
91.9737 |
76.2409 |
69.9806 |
67.3539 |
66.1457 |
|
III |
188.3660 |
131.7800 |
109.2380 |
100.2680 |
96.5038 |
94.7726 |
|
0.3 |
I |
103.6020 |
67.3964 |
48.5082 |
38.0498 |
31.9098 |
28.1590 |
II |
134.0900 |
87.2294 |
62.7829 |
49.2469 |
41.3000 |
36.4455 |
|
III |
192.1250 |
124.9820 |
89.9542 |
70.5587 |
59.1716 |
52.2155 |
Table 5. Proportionality factor for simply-supported FG porous plate
Mode |
|
|
|
|
|
|
|
Proportionality factor |
% change |
I |
0.5 |
0 |
0 |
12.3370 |
0 |
0.1 |
12.5139 |
1.0143 |
1.4 |
II |
|
|
|
19.7395 |
|
|
20.0225 |
1.0143 |
1.4 |
III |
|
|
|
32.4210 |
|
|
32.8858 |
1.0143 |
1.4 |
I |
|
|
|
|
1 |
|
9.2033 |
0.7460 |
-25.4 |
II |
|
|
|
|
|
|
14.7255 |
0.7460 |
-25.4 |
III |
|
|
|
|
|
|
24.1858 |
0.7460 |
-25.4 |
I |
|
|
|
|
2 |
|
8.1012 |
0.6567 |
-34.3 |
II |
|
|
|
|
|
|
12.9620 |
0.6567 |
-34.3 |
III |
|
|
|
|
|
|
21.2894 |
0.6567 |
-34.3 |
I |
|
|
|
|
5 |
|
7.5046 |
0.6083 |
-39.2 |
II |
|
|
|
|
|
|
12.0076 |
0.6083 |
-39.2 |
III |
|
|
|
|
|
|
19.7217 |
0.6083 |
-39.2 |
I |
1.0 |
|
|
19.7392 |
0 |
0.1 |
20.0222 |
1.0143 |
1.4 |
II |
|
|
|
49.3480 |
|
|
50.0565 |
1.0143 |
1.4 |
III |
|
|
|
49.3480 |
|
|
50.0565 |
1.0143 |
1.4 |
I |
|
|
|
|
1 |
|
14.7253 |
0.7460 |
-25.4 |
II |
|
|
|
|
|
|
36.8139 |
0.7460 |
-25.4 |
III |
|
|
|
|
|
|
36.8139 |
0.7460 |
-25.4 |
I |
|
|
|
|
2 |
|
12.9619 |
0.6567 |
-34.3 |
II |
|
|
|
|
|
|
32.4053 |
0.6567 |
-34.3 |
III |
|
|
|
|
|
|
32.4053 |
0.6567 |
-34.3 |
I |
|
|
|
|
5 |
|
12.0074 |
0.6083 |
-39.2 |
II |
|
|
|
|
|
|
30.0191 |
0.6083 |
-39.2 |
III |
|
|
|
|
|
|
30.0191 |
0.6083 |
-39.2 |
I |
2.0 |
|
|
49.3480 |
0 |
0.1 |
50.0556 |
1.0143 |
1.4 |
II |
|
|
|
78.9579 |
|
|
80.0899 |
1.0143 |
1.4 |
III |
|
|
|
128.3320 |
|
|
130.1720 |
1.0143 |
1.4 |
I |
|
|
|
|
1 |
|
36.8132 |
0.7460 |
-25.4 |
II |
|
|
|
|
|
|
58.9019 |
0.7460 |
-25.4 |
III |
|
|
|
|
|
|
95.7344 |
0.7460 |
-25.4 |
I |
|
|
|
|
2 |
|
32.4047 |
0.6567 |
-34.3 |
II |
|
|
|
|
|
|
51.8482 |
0.6567 |
-34.3 |
III |
|
|
|
|
|
|
84.2698 |
0.6567 |
-34.3 |
I |
|
|
|
|
5 |
|
30.0185 |
0.6083 |
-39.2 |
II |
|
|
|
|
|
|
48.0302 |
0.6083 |
-39.2 |
III |
|
|
|
|
|
|
78.0645 |
0.6083 |
-39.2 |
Figure 2 shows the effect of the volume fraction index on the first three values of the frequency parameter for .
It is observed that frequency decreases with increasing value of . This is due to the fact that a higher value of introduces more metal components and reduces the stiffness of the plate, i.e., elasticity modulus and bending rigidity. The variation of non-dimensional frequency with porosity volume fraction for is shown in Fig. 3.
The frequency decreases with increasing value of . With the increase in , the strength of the material decreases. It is concluded that even porosity distribution lowers the natural frequency.
The effect of aspect ratio on frequency for is shown in Fig. 4 and it is observed that frequency increases with increasing value of .
Fig. 5 demonstrates the frequency-response variation with for The frequency first increases and then becomes constant.
The variation of , i.e., the distance between the physical neutral surface and the geometrical mid-plane with porosity volume fraction k for different values of volume fraction index is shown in Fig. 6.
The value of increases with the increase in k. It is also observed that the value of for remains lower than that for up to k=0.09 and remains higher for k >0.09.
|
Fig. 2. Frequency parameter of isotropic FG porous plate for : First mode , |
|
Fig. 3. Frequency parameter of isotropic FG porous plate for : First mode , |
|
Fig. 4. Frequency parameter of isotropic FG porous plate for : First mode , |
|
Fig. 5 Frequency parameter of isotropic FG porous plate : First mode , Second mode , Third mode |
|
Fig. 6 Variation of with volume fraction index g for different values of porosity volume fraction k; |
The value of for remains lower than that for up to and remains higher for k>0.16. Variation of proportionality factor with is shown in Fig. 7.
The first three mode shapes for FG porous square plate are shown in Fig. 8.
|
Fig. 7 Variation of proportionality factor with for simply-supported FG porous plate without restraint edges for k=0.1 (□), k=0.2 (∆), k=0.3 (O) |
|
Fig. 8 First three mode shapes for FG porous square plate for |
Free transverse vibration of a thin isotropic FG rectangular porous plate is studied here. A simply-supported plate having all the edges elastically restrained against rotation is considered. Material properties are assumed to be graded in the thickness direction and are dependent on even porosity distribution. The first three frequencies are obtained using the Rayleigh-Ritz method and boundary characteristic orthogonal polynomials. The effects of volume fraction index, porosity volume index, aspect ratio, and restraint parameters are studied on the frequencies. It is concluded that
The results presented here may serve as a benchmark for further studies dealing with FG porous rectangular plates with elastically restrained edges.
Nomenclature
|
Length of the plate |
|
Breadth of the plate |
|
Volume fraction index |
|
Thickness of the plate |
|
Porosity volume fraction |
|
Time |
|
Displacement |
|
Order of approximation |
|
Strain and kinetic energies of the plate |
|
Young’s modulus |
|
Young’s modulus of metal |
|
Young’s modulus of ceramic |
|
Rotational spring constants |
|
Maximum strain and kinetic energies of the plate |
|
Maximum strain energy associated to the rotational restraints |
|
Maximum transverse displacement |
|
Density of the plate material |
|
Poisson’s ratio |
|
Frequency parameter |
|
Aspect ratio |
|
Circular frequency |
|
Density of metal |
|
Density of ceramic |
|
Distance between the geometrical mid-plane and the physical neutral surface |
|
Normal and shear strains |
|
Normal and shear stresses |
|
jth Orthogonal polynomial |
|
jth Orthonormal polynomial |
|
The Kronecker delta |
Acknowledgments
The author is thankful to the learned reviewers for their constructive comments.
Conflicts of Interest
The author declares that there is no conflict of interest regarding the publication of this manuscript.
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