Static Buckling and Free Vibration Analysis of Bi-Dimensional FG Metal Ceramic Porous Beam

Document Type : Research Article

Authors

Department of Mechanical Engineering, Faculty of Engineering, Arak University, Arak, 38156-88349, Iran

Abstract

This study presents an analytical solution for static buckling and free vibration analysis of bi-dimensional functionally graded (2D-FG) metal-ceramic porous beams. To achieve this goal, equations of motion for the beam are derived by using Hamilton's principle and then the derived equations were solved in the framework of Galerkin’s well-known analytical method for solution of equations. The material properties of the beam are variable along with thickness and length according to the power-law function. During the fabrication of functionally graded materials (FGMs), porosities may occur due to technical problems causing micro-voids to appear. Detailed mathematical derivations are presented and numerical investigations are performed, while emphasis is placed on investigating the effect of various parameters such as FG power indexes along both directions of thickness and length, porosity, and slenderness ratios (L/h), on the non-dimensional frequency and static buckling of the beam based on new higher deformation beam theory. The accuracy of the proposed model is validated based on comparisons of the results with the accepted studies. According to the result in both buckling and vibration analysis, the presented modified transverse shear stress along the thickness has shown closer consequences in comparison with TBT.

Keywords

Main Subjects


Static Buckling and Free Vibration Analysis of Bi-Dimensional FG Metal Ceramic Porous Beam

  1. Shabani, P. Mehdianfar, K. Khorshidi *

Department of Mechanical Engineering, Faculty of Engineering, Arak University, Arak, 38156-88349, Iran

 

KEYWORDS

 

ABSTRACT

Porosity;

Computational analysis;

2D-FGM;

Composite materials;

Buckling.

This study presents an analytical solution for static buckling and free vibration analysis of bi-dimensional functionally graded (2D-FG) metal-ceramic porous beams. To achieve this goal, equations of motion for the beam are derived by using Hamilton's principle and then the derived equations were solved in the framework of Galerkin’s well-known analytical method for solution of equations. The material properties of the beam are variable along with thickness and length according to the power-law function. During the fabrication of functionally graded materials (FGMs), porosities may occur due to technical problems causing micro-voids to appear. Detailed mathematical derivations are presented and numerical investigations are performed, while emphasis is placed on investigating the effect of various parameters such as FG power indexes along both directions of thickness and length, porosity, and slenderness ratios (L/h), on the non-dimensional frequency and static buckling of the beam based on new higher deformation beam theory. The accuracy of the proposed model is validated based on comparisons of the results with the accepted studies. According to the result in both buckling and vibration analysis, the presented modified transverse shear stress along the thickness has shown closer consequences in comparison with TBT.

 

 

1.     Introduction

In recent years, a new class of composite materials formed that contained two or more phases which are known as functionally graded materials (FGMs). FGMs are made of two or more substances whose characteristics vary continuously from one direction to another. The performances and advantages of FGMs have led to their increasing use in many sectors including hi-tech industries, aerospace, naval, automotive, and civil structures[1]. An important application of FGM in structural components is in beams and beam structures. To support the growing use of FGM beams, the study of their vibration behavior becomes necessary. In recent years, the analysis of the free vibration of FGM beams has been performed using different analytical and numerical methods[2]. buckling and free vibration of a curved Timoshenko FG microbeam is studied by Rahmani et al. [3] based on strain gradient theory (SGT) theory. Compared to conventional materials, porous materials possess both remarkable design flexibility and significant applicability across diverse fields. Consequently, numerous researchers have dedicated their efforts to exploring various porous structures. For instance, Ghasemi and Meskini [4] conducted an investigation into the free vibration analysis of porous laminated rotating circular cylindrical shells. Several studies have been carried out on the behaviors of functionally graded material in recent years [5-10]. Atashipour et al. [11] developed a closed-form 2D elasticity solution for stresses and displacements of a curved FG beam subjected to a shear force. Among the earliest investigators in this field, Masjedi et al. [12], conducted a large deflection of functionally graded porous beams based on a geometrically exact theory. The buckling behavior of engineering structures made of advanced materials has been investigated by many researchers[13-18]. Buckling of Sandwich Structures with Metamaterials Core Integrated by Graphene Nanoplatelets Reinforced Polymer Composite was analyzed by Shabani and Khorshidi[19]. The analytical solution presented by Dym and Williams [20] can be used to estimate the buckling behavior of curved beams. The nondeterministic vibration frequencies and mode shapes of FG porous beams were investigated by Gao et al. [21] using a hybrid Chebyshev surrogate model with a discrete singular convolution method. Large amplitude nonlinear vibration analysis of functionally graded porous Timoshenko beams is examined by Ebrahimi and Zia [22]. Chen et al. [23] investigated free vibration and transient analyses of functionally graded piezoelectric materials curved Timoshenko beams in their work. Mahmoodabadi et al. [24] used a multi-objective optimization process based on the genetic algorithm to study damping the vibrations of a piezo-actuating composite beam. The Peridynamics analytical solutions for the buckling load of beams with various boundary conditions were introduced by Yang et al. [25]. Ly et al. [26] used different hybrid ML models to predict the critical buckling load of I-shaped cellular steel beams with circular openings.

In this study, the effects of variable L/h, porosity coefficient, and gradient indexes in two directions on natural frequency and critical buckling load of 2D-FG porous beams have been investigated. Young’s modulus, mass density, and Poisson's ratio of the beam are assumed to vary along the thickness and length of the beam according to power-laws form and also, they are influenced by the porosity. In this study to achieve better accuracy, modified transverse shear stress has been presented and compared with other theories. In the following, the higher-order governing equations are derived by using Hamilton's principle. In the end, the Galerkin method is employed to solve them, and the non-dimensional frequencies and critical buckling loads are obtained.

2.     Problem and Formulation

2.1. Two Dimensionally Functionally Graded Porous Beams

Consider a beam as shown in Fig. 1. with length L, width b, and thickness h, with Cartesian coordinate system O(x y z) which the origin of coordinate system O is chosen at the left of the beam. The Mechanical properties of the beam, such as Young's modulus E(x, z), shear modulus G(x, z), Poisson's modulus υ(x, z) and mass density ρ(x, z) with the material properties can be varying along length and thickness like Fig. 1.

 

Fig. 1. Geometry of 2D-FG beam.

The effective material properties(P) can be expressed by using the rule of mixture:

 

(1)

 

(2)

where Pc and Pm are epitomes of mechanical properties and Rc and Rm are volume fractions of ceramic and metal. Substitution of Eq. (2) into Eq. (1), the material properties of the 2D-FG beam are obtained as [27]:

 

(3)

As shown in Fig. 2, it is assumed that the porosities in the x and z directions are distributed uniformly. The effective material properties of the even porosity are defined as:

 

(4)

where  is a porous parameter or porosity volume fraction.

 

Fig. 2. Porosity of beam.

The assumed beam is graded from metal at the lower left corner edge to ceramic at the top right corner edge (Fig. 1). The volume fraction of ceramic material is given by:

 

(5)

The kx and kz are the power-law of the beam which ascertain properties in length and thickness direction. The mechanical properties of the 2D-FG porous beam can be written as [28]:

 

(6a)

 

(6b)

 

(6c)

2.2. Mathematical Modeling

The displacement filed the present shear deformation beam theories, are given as [29]:

 

(7a)

 

(7b)

where u(x) and w(x) respectively represent the axial and transverse displacements for the mid-access, and φ is the rotation of the cross-sections. Assuming infinitesimal deformations, strain-displacement relations are[30]:

 

(8a)

 

(8b)

The stress-strain relations by using Hook's law can be defined as follows:

 

(9a)

 

(9b)

E and G represent the modulus of elasticity and shear moduli, respectively, while ks denotes the shear correction factor. Where the shear modulus (G) is [31]:

 

(10)

Hamilton's principle is employed to extract equations of motion [32, 33].

 

(11)

where U and T are the strain and kinetic energy, respectively of the beam.  is the variation operator. The strain energy of the beam(U) is calculated as follows [34, 35]:

 

(12)

Finally, variation of strain energy with respect to u(x), w(x) and  is shown as.

 

(13)

where Axx, Axz, Bxx, Dxx, Sxz, and Txz are defined by:

 

(14a)

 

(14b)

 

(14c)

The kinetic energy is obtained as [36]:

 

(15)

The inertia coefficients appearing in Eq. 19 can be defined as:

 

(16)

Finally, the total variation of kinetic energy associated with the sandwich beam in the integral form as:

 

(17)

By substituting strain energy Eq. (13) and kinetic energy Eq. (17) into Hamilton's principal Eq. (11), equations of motion may be expressed as Eqs. (18a) – (18c).

 

(18a)

 

(18b)

 

(18c)

2.3. Analytical Solution

To obtain the theoretical solution, the Galerkin method is considered. According to this method, the displacements functions u(x, t), w(x, t) and  are assumed as follows[37]:

 

(19a)

 

(19b)

 

(19c)

where ,  and are unknown coefficients that will be determined. i = , K denotes the order of series and  is the natural frequency. ,  and are the admissible functions that satisfy the fully clamped boundary conditions.

 

(20a)

 

(20b)

 

(20c)

Free vibration analysis of the bi-dimensional functionally graded sandwich beam can be computed from Eq. (21a)[38]. Also, the amount of critical buckling loads will be calculated by Eq. (21b):

 

(21a)

 

(21b)

where M is the global mass matrix, K is the stiffness matrix and unknown coefficients of Eq. (21) is .

3.     Numerical Results and Discussion

In this section, the free vibration of the 2D-FG porous beam with respect to porosity coefficients ( ) is studied. Functionally graded material composed of a mixture of alumina and steel as ceramic and metal respectively with the material. Their properties are given in Table 1. The influence of different slenderness ratios, L/h = 5, 10, 15, and 20 on the non-dimensional natural frequency are investigated. The shear correction factor for TBT theory is considered as ks = 5/6 [39].

Table 1. Properties of materials[37]

Material

Elasticity module (E)

Mass density (ρ)

Poisson's ratio (υ)

Alumina

380

3800

0.23

Steel

70

2700

0.23

The dimensionless fundamental frequency and critical buckling load are defined as Eq. 22.

 

(22a)

 

(22b)

where I represent the moment of inertia and A represents the area of the cross-section of the beam.

 

(23)

In this research, the solution is calculated for different the power-law index between 0 and 10 moreover, porosity coefficients are taken as
 0, 0.1, and 0.2. The total thickness of the beam (h) is constant and it is 0.1 m. The function indexes (p0 and q0), are taken as 2 for satisfying the clamped-clamped boundary condition. Besides, g(z) and f(z) are related parameters to the beam's theory, as they take as 0 and z for TBT, and z and  for NHOBT [40], respectively. Validation of our formulation and the results are obtained and compared with the results of Ref. [41], [42], and [43]. In Table 2, the first frequency of FG porous less beam with
L/h = 5 and kx = 0 are calculated and they will be compared with references. To verify our new theory, the natural frequency of the FG beam with a greater slender ratio in Table 3 is calculated.

In addition, another comparison with ref [41] and [43] is presented to show the accuracy of the new higher shear deformation beam theory to calculate the critical buckling load. The mechanical properties of the pure beam have changed along the z direction and the ratio of beam's length to height is 10. The results are written in Table 4.

The amounts of Ncr of the FG beam with NHOBT and L/h = 5 are reported in Table 5. By checking both tables, it is clear that there is accuracy and agreement between the references and the present study. Thus, the results of natural frequencies and critical buckling loads will be published under effective parameters such as L/h, porosity (η), and functionally graded power indexes (kx and kz).

The results of non-dimensional frequencies of a two-dimensional functionally graded porous beam with several η, kx, and kz by using two theories are written in Table 6. The amount of ϖ has been reduced by approximately 37% by changing kz from 0 to 8. On the other hand, the variation of kx has affected ϖ by around 34%, indicating that kz has a greater impact on the results. Additionally, by changing η from 0 to 0.2, the amount of ϖ has increased by approximately 3%.

The amount of Ncr under changing kx, kz, and η with TBT and NHOBT is calculated and the consequences are written in Table 7. By changing kz and kx between 0 to 8, the amount of Ncr has reduced by about 76 and 69 % respectively. The factor with the greatest impact on the results is kz, with approximately 7% more effect. Furthermore, the Ncr decreased by about 11% with increasing η from 0 to 0.2.

 

Table 2. Comparison of the dimensionless natural frequencies (l/h = 5 and η = 0)

 

kz = 0

kz = 1

kz = 2

kz = 5

kz = 10

Present (NHOBT)

10.2285

8.0969

7.3290

6.6448

6.3042

Present (TBT)

10.2579

8.1098

7.3750

6.7128

6.4759

Thuc et al. HOBT [41]

10.0678

7.9522

7.1801

6.4961

6.1662

Thuc et al. FOBT [41]

9.9984

7.9015

7.1901

6.6447

6.3161

Simsek HOBT [42]

10.0705

7.9503

7.1767

6.4935

6.1652

Simsek FOBT [42]

10.0344

7.9253

7.2113

6.6676

6.3406

Table 3. Comparison of the dimensionless natural frequencies (l/h = 20 and η = 0)

 

kz = 0

kz = 1

kz = 2

kz = 5

kz = 10

Present (NHOBT)

12.2418

9.4918

8.6778

8.2159

7.9342

Thuc et al. HOBT [41]

12.2228

9.4328

8.5994

8.1460

7.8862

Thuc et al. FOBT [41]

12.2202

9.4311

8.6047

8.1698

7.9115

Simsek HOBT [42]

12.2238

9.4315

8.5975

8.1446

7.8858

Simsek FOBT [42]

12.2235

9.4314

8.6040

8.1699

7.9128

Table 4. Comparison of the results of critical buckling load (l/h = 10 and η = 0)

 

kz = 0

kz = 1

kz = 2

kz = 5

kz = 10

Present (NHOBT)

194.4026

98.8053

76.8331

62.9629

56.4158

Li and Batra [43]

195.3400

98.7490

76.9800

64.0960

57.7080

Thuc et al. FOBT [41]

195.3730

98.7923

77.0261

64.1324

57.7329

Thuc et al. HOBT [41]

195.3610

98.7868

76.6677

62.9786

56.5971

Table 5. Comparison of the results of critical buckling load (l/h = 5 and η = 0)

 

kz = 0

kz = 1

kz = 2

kz = 5

kz = 10

Present (NHOBT)

152.1990

79.8063

61.2369

47.116

41.1128

Li and Batra [43]

154.3500

80.4980

62.6140

50.3840

44.2670

Thuc et al. FOBT [41]

154.4150

80.5480

62.6616

50.4207

44.2946

Thuc et al. HOBT [41]

154.5500

80.6087

61.7925

47.7562

41.8042

Table 6. First non-dimensional frequency (ϖ) of 2D-FG porous beam for various kx, kz, and η (L/h = 10).

Theory

η

kz

kx

0

1

2

4

6

8

TBT

0

0

21.6960

17.0553

15.6524

14.5606

14.0223

13.6403

1

16.8500

14.3819

13.6517

13.0863

12.7849

12.5764

2

15.3637

13.6340

13.0914

12.6367

12.4165

12.2903

4

14.6350

13.2308

12.7760

12.3834

12.1918

12.0892

6

14.3520

13.0449

12.6168

12.2521

12.0960

11.9658

8

14.1373

12.8873

12.4975

12.1511

12.0043

11.9063

NHOBT

0

0

21/1618

16/6429

15/3731

14/2928

13/7558

13/3948

1

16/5051

14/0453

13/3743

12/8050

12/5325

12/3574

2

15/0571

13/3139

12/8158

12/3854

12/1817

12/0524

4

14/2740

12/8894

12/4747

12/1139

11/9551

11/8567

6

13/9665

12/6941

12/3101

11/9907

11/8451

11/7547

8

13/7419

12/5464

12/1924

11/8892

11/7570

11/6799

TBT

0.1

0

21.9998

16.7114

15.0772

13.6923

13.0121

12.5896

1

16.5388

13.6219

12.7145

12.0111

11.6668

11.4278

2

14.6162

12.6623

12.0187

11.4848

11.2217

11.0879

4

13.6436

12.1432

11.6160

11.1728

10.9759

10.8546

6

13.3410

11.9406

11.4468

11.0374

10.8555

10.7441

8

13.1444

11.7965

11.3355

10.9355

10.7829

10.6676

NHOBT

0.1

0

22/3579

16/9650

15/3647

14/0096

13/3560

12/9310

1

16/7512

13/8084

12/9738

12/2489

11/9219

11/7106

2

14/8641

12/8713

12/2623

11/7220

11/4849

11/3378

4

13/9234

12/3669

11/8677

11/4237

11/2257

11/1112

6

13/6599

12/1858

11/7091

11/2917

11/1181

11/0058

8

13/4683

12/0397

11/5834

11/1987

11/0331

10/9345

TBT

0.2

0

22.3718

16.2578

13.9010

12.1407

11.3053

10.7474

1

16.0382

12.4432

11.2190

10.2780

9.8109

9.5400

2

13.4114

11.1096

10.2812

9.5863

9.2764

9.0820

4

11.8584

10.3262

9.7099

9.1750

8.9410

8.8175

6

11.4574

10.0734

9.5067

9.0297

8.8242

8.6936

8

11.3014

9.9231

9.3867

8.9382

8.7464

8.6273

NHOBT

0.2

0

22/7021

16/3349

14/2677

12/4383

11/6037

11/0778

1

16/2534

12/5477

11/4541

10/4811

10/0477

9/7799

2

13/6285

11/2567

10/4767

9/7967

9/4873

9/3149

4

12/0916

10/4981

9/9149

9/3829

9/1574

9/0258

6

11/7261

10/2714

9/7284

9/2452

9/0443

8/9243

8

11/5545

10/1302

9/6076

9/1525

8/9648

8/8529

Table 7. Critical buckling load (Ncr) of 2D-FG porous beam for various kx, kz, and η (L/h = 10).

Theory

η

kz

kx

0

1

2

4

6

8

TBT

0

0

201.3001

101.2443

73/3782

56/8435

51/2608

48/3640

1

101.8384

66.6279

55/4769

47/7935

44/9744

43/4770

2

79.3865

58.3191

50/8079

45/2804

43/1927

42/0855

4

68.2815

53.5313

47/9427

43/6789

42/0411

41/1664

6

64.3308

51.4026

46/5823

42/8864

41/4587

40/6963

8

61.6250

49.8626

45/5830

42/2954

41/0188

40/3319

NHOBT

0

0

195/3779

97/2664

71/2192

55/4709

50/1329

47/3546

1

99/2310

64/5146

53/9762

46/6343

43/9498

42/5304

2

77/1877

56/4267

49/3866

44/1401

42/1719

41/1327

4

65/7422

51/5953

46/4741

42/5032

40/9942

40/1957

6

61/5646

49/4644

45/1055

41/7020

40/4027

39/7119

8

58/8715

47/9899

44/1322

41/1171

39/9625

39/3461

TBT

0.1

0

189/7017

86/5973

58/2271

42/5622

37/4739

34/8816

1

88/0537

52/9688

41/9996

34/7625

32/1893

30/8440

2

64/0969

44/5446

37/5045

32/4321

30/5622

29/5826

4

52/5693

39/8829

34/8210

30/9839

29/5379

28/7694

6

49/1145

38/0454

33/6697

30/3341

29/0618

28/3879

8

46/9595

36/7694

32/8503

29/8570

28/7108

28/1008

NHOBT

0.1

0

184/1132

82/7353

56/4400

41/5326

36/6694

34/1715

1

85/8718

51/1773

40/8558

33/9401

31/4780

30/1892

2

62/4375

43/0432

36/4529

31/6364

29/8622

28/9356

4

50/6270

38/3560

33/7335

30/1575

28/8153

28/1133

6

46/8667

36/4948

32/5662

29/4938

28/3337

27/7230

8

44/6357

35/2597

31/7613

29/0213

27/9825

27/4327

TBT

0.2

0

178/0717

70/4071

40/9069

26/8716

22/6228

20/5068

1

73/6780

38/2597

27/4892

20/9948

18/8072

17/6832

2

47/4333

29/7059

23/3508

18/9993

17/4592

16/6723

4

34/6064

25/0341

20/8595

17/7380

16/5918

16/0017

6

31/5006

23/5343

19/9695

17/2607

16/2562

15/7359

8

30/0213

22/6233

19/3964

16/9431

16/0272

15/5484

NHOBT

0.2

0

172/8112

66/3052

39/5456

26/1841

22/1330

20/0973

1

71/9500

36/7506

26/6959

20/4944

18/4025

17/3281

2

46/3571

28/6013

22/6763

18/5411

17/0741

16/3237

4

33/4452

23/9716

20/1835

17/2666

16/1973

15/6521

6

30/0084

22/4247

19/2647

16/7747

15/8535

15/3803

8

28/3175

21/5147

18/6904

16/4552

15/6238

15/1932

 

 

The beam is made of two-dimensional functionally graded material; thus, it has been influenced by FG power indexes in x (kx) and z (kz) directions. The critical buckling loads (Ncr) and the natural frequencies (ϖ) of the beam are related to the kx and kz. In Figure 3a, the relation between ϖ and FG power indexes in a porous less beam is shown, the ratio of length to the height of the beam is considered as 10. In Figure 3b, the effect of FG power indexes on Ncr of the porous beam is under new theory (NHOBT) with η = 0.2 and L/h = 10 illustrated. Generally, the amount of Ncr and ϖ have reduced with increasing the FG power indexes. However, Ncr has been affected more than ϖ by changing kx and kz. In the high amount of FG power indexes the variations of Ncr have been moved to near 0. On the other hand, the ϖ has been diminished continuously by reducing the kx and kz. Power indexes affect how material properties vary along the length and thickness directions, which influence their stiffness and mass distribution. A higher FG power index reduces the effective stiffness and increases the effective mass of a beam.

 

Fig. 3a. Non-dimensional frequency of 2D-FG porous beam for various kz and kx (TBT, L/h = 10 and η = 0)

 

Fig. 3b. Critical buckling load of 2D-FG porous beam for various kz and kx (NHOBT, L/h = 10 and η = 0.2)

The impact of various ratios of the beam's spin to its height on ϖ and Ncr is shown in Figure 4. A beam with n = 0.1 and kx = 1 is used to analyze the three amounts of L/h = 5, 10, and 20 on the ϖ in the first part of the Figure. A direct connection is seen between the amount of L/h and the ϖ. Additionally, the same study on Ncr has been conducted under unique conditions using a new theory. The results of this study are plotted in Figure 4b and the amount of Ncr has been rose by growing the L/h from 5 to 20. Also, the effect of L/h = 5 on the Ncr and ϖ is higher than 10 and 20. Reducing the strain energy will decrease the bending moment of the beam, so when the L/h is going to be diminished, the amount of Ncr and ϖ will be reduced. A higher slenderness ratio means a longer and thinner beam, which is more flexible and less stiff than a shorter and thicker beam.

 

Fig. 4a. Comparison of non-dimensional frequency of
 2D-FG porous beam for various slenderness ratios
 (L/h) (η = 0.1 and kx = 1)

 

Fig. 4b. Comparison of Critical buckling load of
2D-FG porous beam for various height to span ratios (L/h) (NHOBT, η = 0.1 and kx = 1)

Another important and effective parameter is porosity. Figure 5 shows the effect of η = 0, 0.1, and 0.2 on the Ncr and ϖ. When the amount of η is 0, the beam does not have any porosity. In the constant kz and kz, the ϖ has shown an inverse direction with η so as to by increasing the η, ϖ has fallen. The same relation is seen between η and Ncr, however, the effect on Ncr is bolder than on ϖ. By reducing the stiffness of the beam, the amount of ϖ and Ncr will be influenced and decreased. Porosity affects the material density and strength along the thickness direction of beams, which in turn affects their stiffness and mass. Higher porosity means more voids or holes in the material, which reduces its weight and resistance to deformation. A higher porosity reduces the effective stiffness and increases the effective mass of a beam under both axial and transverse loading, which lowers its critical buckling load and natural frequency.

 

Fig. 5a. Effect of various porosity(η) on non-dimensional frequency of 2D-FG porous beam (L/h = 10 and kx = 1)

 

Fig. 5b. Effect of various porosity(η) on Critical buckling load of 2D-FG porous beam (NHOBT, L/h = 10 and kx = 8)

4.     Conclusions

In this research paper, we have investigated the impact of various parameters, including porosity (η), slenderness ratios (L/h), and power-law indexes (kx and kz) in both axial and thickness directions, on the natural frequencies and critical buckling load of 2D-FG porous beams. We have utilized a new higher-order beam theory to analyze these effects.

Our findings demonstrate that the power-law indexes (kx and kz) play a significant role in determining the natural frequencies. Increasing the FG power indexes leads to a decrease in the values of the natural frequencies (Ncr) and the critical buckling load (ϖ). This can be explained by the change in material properties along the beam's axial and thickness directions. The power-law indexes alter the distribution of the constituent materials, affecting their stiffness and density. Higher power-law indexes result in a more significant variation of material properties, leading to decreased natural frequencies and critical buckling loads. In the case of high power-law indexes, the variations in Ncr do not exhibit significant changes. Additionally, when considering a constant value for kx and kz, we observe an inverse relationship between the porosity (η) and ϖ. As η increases, ϖ decreases, and the same trend is observed between η and Ncr. This behavior can be attributed to the presence of voids or pores within the material. The presence of voids weakens the overall structural integrity and reduces the effective stiffness of the beam. As a result, the natural frequencies decrease, and the critical buckling load is diminished. Furthermore, frequencies and critical buckling loads are more sensitive to porosity in high power-law indexes. A direct connection is seen between the amount of L/h and the ϖ. The amount of Ncr has been rose by growing the L/h from 5 to 20. Also, the effect of L/h = 5 on the Ncr and ϖ is higher than 10 and 20.

These findings provide valuable insights into the behavior of bi-dimensional FG metal ceramic porous beams and highlight the importance of considering porosity, slenderness ratios, and power-law indexes in their design and analysis. Further research in this area can contribute to the development of more efficient and reliable structures with improved performance characteristics.

Conflicts of Interest

The author declares that there is no conflict of interest regarding the publication of this manuscript. In addition, the authors have entirely observed the ethical issues, including plagiarism, informed consent, misconduct, data fabrication and/or falsification, double publication and/or submission, and redundancy.

References

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[2]   Ramteke, P.M. & Panda, S.K., 2023. Computational modelling and experimental challenges of linear and nonlinear analysis of porous graded structure: A comprehensive review. Archives of Computational Methods in Engineering, 30 (5), pp.3437-3452.

[3]   Rahmani, O., Hosseini, S.a.H., Ghoytasi, I. & Golmohammadi, H., 2016. Buckling and free vibration of shallow curved micro/nano-beam based on strain gradient theory under thermal loading with temperature-dependent properties. Applied Physics A, 123 (1), pp.4.

[4]   Ghasemi, A.R. & Meskini, M., 2019. Free vibration analysis of porous laminated rotating circular cylindrical shells. Journal of Vibration and Control, 25 (18), pp.2494-2508.

[5]   Khorshidi, K., Bahrami, M., Karimi, M. & Ghasemi, M., 2020. A theoretical approach for flexural behavior of fg vibrating micro-plates with piezoelectric layers considering a hybrid length scale parameter. Journal of Theoretical and Applied Vibration and Acoustics, 6 (1), pp.51-68.

[6]   Zhu, C. & Xu, S.P., 2018. Nonlinear free vibration analysis of fg tubes conveying fluid. Zhendong yu Chongji/Journal of Vibration and Shock, 37, pp.195-201 and 247.

[7]   Bouafia, H., Abdelbaki, C., Bousahla, A., Bourada, F., Heireche, H., Tounsi, A., Benrahou, K., Tounsi, A., Al-Zahrani, M. & Hussain, M., 2021. Natural frequencies of fgm nanoplates embedded in an elastic medium. Advances in Nano Research, 11.

[8]   Hidayat, M.I.P., 2022. A meshless thermal modelling for functionally graded porous materials under the influence of temperature dependent heat sources. Engineering Analysis with Boundary Elements, 145, pp.188-210.

[9]   Alavi, S.K., Ayatollahi, M.R., Petrů, M. & Koloor, S.S.R., 2022. On the dynamic response of viscoelastic functionally graded porous plates under various hybrid loadings. Ocean Engineering, 264, pp.112541.

[10] El Khouddar, Y., Adri, A., Outassafte, O., Rifai, S. & Benamer, R., 2021. Non-linear forced vibration analysis of piezoelectric functionally graded beams in thermal environment. International Journal of Engineering, 34 (11), pp.2387-2397.

[11] Atashipour, S.R., Nasr, A. & Fadaee, M., 2010. An elasticity solution for static analysis of functionally graded curved beam subjected to a shear force. International Journal of Engineering, 23 (2), pp.169-178.

[12] Khaneh Masjedi, P., Maheri, A. & Weaver, P.M., 2019. Large deflection of functionally graded porous beams based on a geometrically exact theory with a fully intrinsic formulation. Applied Mathematical Modelling, 76, pp.938-957.

[13] Emam, S. & Lacarbonara, W., 2022. A review on buckling and postbuckling of thin elastic beams. European Journal of Mechanics - A/Solids, 92, pp.104449.

[14] Zhao, H., Li, K., Han, M., Zhu, F., Vázquez-Guardado, A., Guo, P., Xie, Z., Park, Y., Chen, L., Wang, X., Luan, H., Yang, Y., Wang, H., Liang, C., Xue, Y., Schaller, R.D., Chanda, D., Huang, Y., Zhang, Y. & Rogers, J.A., 2019. Buckling and twisting of advanced materials into morphable 3d mesostructures. Proceedings of the National Academy of Sciences, 116 (27), pp.13239-13248.

[15] Ghasemi, A.R., Kiani, S. & Tabatabaeian, A., 2020. Buckling analysis of fml cylindrical shells under combined axial and torsional loading. Mechanics Of Advanced Composite Structures, 7 (2), pp.263-270.

[16] Ghasemi, A.R. & Soleymani, M., 2021. A new efficient buckling investigation of functionally graded cnt/fiber/polymer/metal composite panels exposed to hydrostatic pressure considering simultaneous manufacturing-induced agglomeration and imperfection issues. The European Physical Journal Plus, 136 (12), pp.1220.

[17] Bridjesh, P., Geetha, N.K. & Reddy, G.C.M., 2023. On numerical investigation of buckling in two-directional porous functionally graded beam using higher order shear deformation theory. Mechanics Of Advanced Composite Structures, 10 (2), pp.393-406.

[18] Reddy, G.C.M. & Kumar, N.V., 2023. Free vibration analysis of 2d functionally graded porous beams using novel higher-order theory. Mechanics Of Advanced Composite Structures, 10 (1), pp.69-84.

[19] Shabani, Y. & Khorshidi, K., 2023. Buckling analysis of sandwich structures with metamaterials core integrated by graphene nanoplatelets reinforced polymer composite. Mechanics Of Advanced Composite Structures, 10 (1), pp.1-10.

[20] Dym, C.L. & Williams, H.E., 2011. Stress and displacement estimates for arches. Journal of structural engineering, 137 (1), pp.49-58.

[21] Gao, K., Li, R. & Yang, J., 2019. Dynamic characteristics of functionally graded porous beams with interval material properties. Engineering Structures, 197, pp.109441.

[22] Ebrahimi, F. & Zia, M., 2015. Large amplitude nonlinear vibration analysis of functionally graded timoshenko beams with porosities. Acta Astronautica, 116, pp.117-125.

[23] Chen, M., Chen, H., Ma, X., Jin, G., Ye, T., Zhang, Y. & Liu, Z., 2018. The isogeometric free vibration and transient response of functionally graded piezoelectric curved beam with elastic restraints. Results in Physics, 11, pp.712-725.

[24] Mahmoodabadi, M.J., Mortazavi Yazdi, S.M. & Barani, A., 2020. Vibration damping of piezo actuating composite beams based on the multi-objective genetic algorithm. Journal of Theoretical and Applied Vibration and Acoustics, 6 (2), pp.325-336.

[25] Yang, Z., Naumenko, K., Altenbach, H., Ma, C.-C., Oterkus, E. & Oterkus, S., 2022. Beam buckling analysis in peridynamic framework. Archive of Applied Mechanics, 92.

[26] Ly, H.-B., Le, T.-T., Le, L., Van Quan, T., Vương, L., Thi Vu, H.-L., Nguyen, Q. & Pham, B., 2019. Development of hybrid machine learning models for predicting the critical buckling load of i-shaped cellular beams. Applied Sciences, 9, pp.5458.

[27] Gupta, S. & Chalak, H.D., 2023. Buckling analysis of functionally graded sandwich beam based on third-order zigzag theory. Mechanics Of Advanced Composite Structures, 10 (1), pp.55-68.

[28] Shahsavari, D., Shahsavari, M., Li, L. & Karami, B., 2018. A novel quasi-3d hyperbolic theory for free vibration of fg plates with porosities resting on winkler/pasternak/kerr foundation. Aerospace Science and Technology, 72, pp.134-149.

[29] Reddy, J.N., 2011. Microstructure-dependent couple stress theories of functionally graded beams. Journal of the Mechanics and Physics of Solids, 59 (11), pp.2382-2399.

[30] Wattanasakulpong, N. & Chaikittiratana, A., 2015. Flexural vibration of imperfect functionally graded beams based on timoshenko beam theory: Chebyshev collocation method. Meccanica, 50 (5), pp.1331-1342.

[31] Katili, A.M. & Katili, I., 2020. A simplified ui element using third-order hermitian displacement field for static and free vibration analysis of fgm beam. Composite Structures, 250, pp.112565.

[32] Ghasemi, A.R. & Mohandes, M., 2020. Free vibration analysis of micro and nano fiber-metal laminates circular cylindrical shells based on modified couple stress theory. Mechanics of Advanced Materials and Structures, 27 (1), pp.43-54.

[33] Nejati, M., Ghasemi-Ghalebahman, A., Soltanimaleki, A., Dimitri, R. & Tornabene, F., 2019. Thermal vibration analysis of sma hybrid composite double curved sandwich panels. Composite Structures, 224, pp.111035.

[34] Khorshidi, K., Taheri, M. & Ghasemi, M., 2020. Sensitivity analysis of vibrating laminated composite rec-tangular plates in interaction with inviscid fluid using efast method. Mechanics of Advanced Composite Structures, 7 (2), pp.219-231.

[35] Khorshid, K. & Farhadi, S., 2013. Free vibration analysis of a laminated composite rectangular plate in contact with a bounded fluid. Composite Structures, 104, pp.176-186.

[36] Shabani, Y. & Khorshidi, K., 2022. Free vibration analysis of rectangular doubly curved auxetic-core sandwich panels integrated with cnt-reinforced composite layers using galerkin method. Journal of Science and Technology of Composites, 8 (3), pp.1686-1677.

[37] Elmeiche, A., Megueni, A. & Lousdad, A., 2016. Free vibration analysis of functionally graded nanobeams based on different order beam theories using ritz method. Periodica Polytechnica Mechanical Engineering, 60 (4), pp.209-219.

[38] Khorshidi, K. & Shabani, Y., 2022. Free vibration analysis of sandwich plates with magnetorheological smart fluid core by using modified shear deformation theory. Journal of Science and Technology of Composites, pp.-.

[39] Şimşek, M. & Al-Shujairi, M., 2017. Static, free and forced vibration of functionally graded (fg) sandwich beams excited by two successive moving harmonic loads. Composites Part B: Engineering, 108, pp.18-34.

[40] Mehdianfar, P., Shabani, Y. & Khorshidi, K., 2022. Natural frequency of sandwich beam structures with two dimensional functionally graded porous layers based on novel formulations. International Journal of Engineering, 35 (11), pp.2092-2101.

[41] Vo, T.P., Thai, H.-T., Nguyen, T.-K., Maheri, A. & Lee, J., 2014. Finite element model for vibration and buckling of functionally graded sandwich beams based on a refined shear deformation theory. Engineering Structures, 64, pp.12-22.

[42] Şimşek, M., 2010. Fundamental frequency analysis of functionally graded beams by using different higher-order beam theories. Nuclear Engineering and Design, 240 (4), pp.697-705.

[43] Li, S.-R. & Batra, R.C., 2013. Relations between buckling loads of functionally graded timoshenko and homogeneous euler–bernoulli beams. Composite Structures, 95, pp.5-9.

[1]   Sharma, N.K. & Bhandari, M., 2018. Applications of functionally graded materials (fgms). International journal of engineering research and technology, 2.
[2]   Ramteke, P.M. & Panda, S.K., 2023. Computational modelling and experimental challenges of linear and nonlinear analysis of porous graded structure: A comprehensive review. Archives of Computational Methods in Engineering, 30 (5), pp.3437-3452.
[3]   Rahmani, O., Hosseini, S.a.H., Ghoytasi, I. & Golmohammadi, H., 2016. Buckling and free vibration of shallow curved micro/nano-beam based on strain gradient theory under thermal loading with temperature-dependent properties. Applied Physics A, 123 (1), pp.4.
[4]   Ghasemi, A.R. & Meskini, M., 2019. Free vibration analysis of porous laminated rotating circular cylindrical shells. Journal of Vibration and Control, 25 (18), pp.2494-2508.
[5]   Khorshidi, K., Bahrami, M., Karimi, M. & Ghasemi, M., 2020. A theoretical approach for flexural behavior of fg vibrating micro-plates with piezoelectric layers considering a hybrid length scale parameter. Journal of Theoretical and Applied Vibration and Acoustics, 6 (1), pp.51-68.
[6]   Zhu, C. & Xu, S.P., 2018. Nonlinear free vibration analysis of fg tubes conveying fluid. Zhendong yu Chongji/Journal of Vibration and Shock, 37, pp.195-201 and 247.
[7]   Bouafia, H., Abdelbaki, C., Bousahla, A., Bourada, F., Heireche, H., Tounsi, A., Benrahou, K., Tounsi, A., Al-Zahrani, M. & Hussain, M., 2021. Natural frequencies of fgm nanoplates embedded in an elastic medium. Advances in Nano Research, 11.
[8]   Hidayat, M.I.P., 2022. A meshless thermal modelling for functionally graded porous materials under the influence of temperature dependent heat sources. Engineering Analysis with Boundary Elements, 145, pp.188-210.
[9]   Alavi, S.K., Ayatollahi, M.R., Petrů, M. & Koloor, S.S.R., 2022. On the dynamic response of viscoelastic functionally graded porous plates under various hybrid loadings. Ocean Engineering, 264, pp.112541.
[10] El Khouddar, Y., Adri, A., Outassafte, O., Rifai, S. & Benamer, R., 2021. Non-linear forced vibration analysis of piezoelectric functionally graded beams in thermal environment. International Journal of Engineering, 34 (11), pp.2387-2397.
[11] Atashipour, S.R., Nasr, A. & Fadaee, M., 2010. An elasticity solution for static analysis of functionally graded curved beam subjected to a shear force. International Journal of Engineering, 23 (2), pp.169-178.
[12] Khaneh Masjedi, P., Maheri, A. & Weaver, P.M., 2019. Large deflection of functionally graded porous beams based on a geometrically exact theory with a fully intrinsic formulation. Applied Mathematical Modelling, 76, pp.938-957.
[13] Emam, S. & Lacarbonara, W., 2022. A review on buckling and postbuckling of thin elastic beams. European Journal of Mechanics - A/Solids, 92, pp.104449.
[14] Zhao, H., Li, K., Han, M., Zhu, F., Vázquez-Guardado, A., Guo, P., Xie, Z., Park, Y., Chen, L., Wang, X., Luan, H., Yang, Y., Wang, H., Liang, C., Xue, Y., Schaller, R.D., Chanda, D., Huang, Y., Zhang, Y. & Rogers, J.A., 2019. Buckling and twisting of advanced materials into morphable 3d mesostructures. Proceedings of the National Academy of Sciences, 116 (27), pp.13239-13248.
[15] Ghasemi, A.R., Kiani, S. & Tabatabaeian, A., 2020. Buckling analysis of fml cylindrical shells under combined axial and torsional loading. Mechanics Of Advanced Composite Structures, 7 (2), pp.263-270.
[16] Ghasemi, A.R. & Soleymani, M., 2021. A new efficient buckling investigation of functionally graded cnt/fiber/polymer/metal composite panels exposed to hydrostatic pressure considering simultaneous manufacturing-induced agglomeration and imperfection issues. The European Physical Journal Plus, 136 (12), pp.1220.
[17] Bridjesh, P., Geetha, N.K. & Reddy, G.C.M., 2023. On numerical investigation of buckling in two-directional porous functionally graded beam using higher order shear deformation theory. Mechanics Of Advanced Composite Structures, 10 (2), pp.393-406.
[18] Reddy, G.C.M. & Kumar, N.V., 2023. Free vibration analysis of 2d functionally graded porous beams using novel higher-order theory. Mechanics Of Advanced Composite Structures, 10 (1), pp.69-84.
[19] Shabani, Y. & Khorshidi, K., 2023. Buckling analysis of sandwich structures with metamaterials core integrated by graphene nanoplatelets reinforced polymer composite. Mechanics Of Advanced Composite Structures, 10 (1), pp.1-10.
[20] Dym, C.L. & Williams, H.E., 2011. Stress and displacement estimates for arches. Journal of structural engineering, 137 (1), pp.49-58.
[21] Gao, K., Li, R. & Yang, J., 2019. Dynamic characteristics of functionally graded porous beams with interval material properties. Engineering Structures, 197, pp.109441.
[22] Ebrahimi, F. & Zia, M., 2015. Large amplitude nonlinear vibration analysis of functionally graded timoshenko beams with porosities. Acta Astronautica, 116, pp.117-125.
[23] Chen, M., Chen, H., Ma, X., Jin, G., Ye, T., Zhang, Y. & Liu, Z., 2018. The isogeometric free vibration and transient response of functionally graded piezoelectric curved beam with elastic restraints. Results in Physics, 11, pp.712-725.
[24] Mahmoodabadi, M.J., Mortazavi Yazdi, S.M. & Barani, A., 2020. Vibration damping of piezo actuating composite beams based on the multi-objective genetic algorithm. Journal of Theoretical and Applied Vibration and Acoustics, 6 (2), pp.325-336.
[25] Yang, Z., Naumenko, K., Altenbach, H., Ma, C.-C., Oterkus, E. & Oterkus, S., 2022. Beam buckling analysis in peridynamic framework. Archive of Applied Mechanics, 92.
[26] Ly, H.-B., Le, T.-T., Le, L., Van Quan, T., Vương, L., Thi Vu, H.-L., Nguyen, Q. & Pham, B., 2019. Development of hybrid machine learning models for predicting the critical buckling load of i-shaped cellular beams. Applied Sciences, 9, pp.5458.
[27] Gupta, S. & Chalak, H.D., 2023. Buckling analysis of functionally graded sandwich beam based on third-order zigzag theory. Mechanics Of Advanced Composite Structures, 10 (1), pp.55-68.
[28] Shahsavari, D., Shahsavari, M., Li, L. & Karami, B., 2018. A novel quasi-3d hyperbolic theory for free vibration of fg plates with porosities resting on winkler/pasternak/kerr foundation. Aerospace Science and Technology, 72, pp.134-149.
[29] Reddy, J.N., 2011. Microstructure-dependent couple stress theories of functionally graded beams. Journal of the Mechanics and Physics of Solids, 59 (11), pp.2382-2399.
[30] Wattanasakulpong, N. & Chaikittiratana, A., 2015. Flexural vibration of imperfect functionally graded beams based on timoshenko beam theory: Chebyshev collocation method. Meccanica, 50 (5), pp.1331-1342.
[31] Katili, A.M. & Katili, I., 2020. A simplified ui element using third-order hermitian displacement field for static and free vibration analysis of fgm beam. Composite Structures, 250, pp.112565.
[32] Ghasemi, A.R. & Mohandes, M., 2020. Free vibration analysis of micro and nano fiber-metal laminates circular cylindrical shells based on modified couple stress theory. Mechanics of Advanced Materials and Structures, 27 (1), pp.43-54.
[33] Nejati, M., Ghasemi-Ghalebahman, A., Soltanimaleki, A., Dimitri, R. & Tornabene, F., 2019. Thermal vibration analysis of sma hybrid composite double curved sandwich panels. Composite Structures, 224, pp.111035.
[34] Khorshidi, K., Taheri, M. & Ghasemi, M., 2020. Sensitivity analysis of vibrating laminated composite rec-tangular plates in interaction with inviscid fluid using efast method. Mechanics of Advanced Composite Structures, 7 (2), pp.219-231.
[35] Khorshid, K. & Farhadi, S., 2013. Free vibration analysis of a laminated composite rectangular plate in contact with a bounded fluid. Composite Structures, 104, pp.176-186.
[36] Shabani, Y. & Khorshidi, K., 2022. Free vibration analysis of rectangular doubly curved auxetic-core sandwich panels integrated with cnt-reinforced composite layers using galerkin method. Journal of Science and Technology of Composites, 8 (3), pp.1686-1677.
[37] Elmeiche, A., Megueni, A. & Lousdad, A., 2016. Free vibration analysis of functionally graded nanobeams based on different order beam theories using ritz method. Periodica Polytechnica Mechanical Engineering, 60 (4), pp.209-219.
[38] Khorshidi, K. & Shabani, Y., 2022. Free vibration analysis of sandwich plates with magnetorheological smart fluid core by using modified shear deformation theory. Journal of Science and Technology of Composites, pp.-.
[39] Şimşek, M. & Al-Shujairi, M., 2017. Static, free and forced vibration of functionally graded (fg) sandwich beams excited by two successive moving harmonic loads. Composites Part B: Engineering, 108, pp.18-34.
[40] Mehdianfar, P., Shabani, Y. & Khorshidi, K., 2022. Natural frequency of sandwich beam structures with two dimensional functionally graded porous layers based on novel formulations. International Journal of Engineering, 35 (11), pp.2092-2101.
[41] Vo, T.P., Thai, H.-T., Nguyen, T.-K., Maheri, A. & Lee, J., 2014. Finite element model for vibration and buckling of functionally graded sandwich beams based on a refined shear deformation theory. Engineering Structures, 64, pp.12-22.
[42] Şimşek, M., 2010. Fundamental frequency analysis of functionally graded beams by using different higher-order beam theories. Nuclear Engineering and Design, 240 (4), pp.697-705.
[43] Li, S.-R. & Batra, R.C., 2013. Relations between buckling loads of functionally graded timoshenko and homogeneous euler–bernoulli beams. Composite Structures, 95, pp.5-9.