Abstract
The present study, for the first time, investigates the vibration and flutter analyses of a doubly curved panel composed of functionally graded porous material contained by piezoelectric layers in supersonic flow. In this regard, the first-order piston theory for aerodynamic loading and Reddy’s third-order shear deformation theory for doubly curved panel analysis is used. The governing equations of motion are obtained using Hamilton’s principle and Maxwell’s equation. The Galerkin method is used to discretize the equations of motion. Three types of piezoelectric layers are used, in both open-circuit and closed-circuit electrical boundary conditions. The FG porous material with three types of porosity structure is investigated, including uniform distribution, X-shaped distribution, and V-shaped distribution. Also, the effect of the power of the FG porous material and the porosity coefficient on the frequencies and the flutter boundaries of spherical, cylindrical, doubly curved shell with \(R_{y} = - R_{x}\) and plate structures are investigated. The comparison of the spherical panel, doubly curved panel, cylindrical panel, and plate shows that the spherical panel has the highest and the plate has the lowest stability regions. Also, as the radius to length of the panel increases, the critical flutter aerodynamic pressure increases and the flutter frequency decreases. Furthermore, the effects of piezoelectricity, electrical and mechanical boundary conditions, geometric parameters, and the radii of curvatures on the flutter boundaries and flutter frequencies of FG porous doubly curved panels are investigated in detail.
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References
Krumhaar, H.: Investigation of the accuracy of linear piston theory when applied to cylindrical shells. AIAA J. (1963). https://doi.org/10.2514/3.1832
Dowell, E.H.: Panel flutter-a review of the aeroelastic stability of plates and shells. AIAA J. 8(3), 385–399 (1970). https://doi.org/10.2514/3.5680
Pidaparti, R.: Flutter analysis of cantilevered curved composite panels. Compos. Struct. 25(1–4), 89–93 (1993). https://doi.org/10.1016/0263-8223(93)90154-I
Cunningham, P.R., White, R.G., Aglietti, G.: The effects of various design parameters on the free vibration of doubly curved composite sandwich panels. J. Sound Vib. 230(3), 617–648 (2000). https://doi.org/10.1006/jsvi.1999.2632
Kumar, L.R., Datta, P., Prabhakara, D.: Dynamic instability characteristics of laminated composite doubly curved panels subjected to partially distributed follower edge loading. Int. J. Solids Struct. 42(8), 2243–2264 (2005). https://doi.org/10.1142/S0219455405001507
Zhang, W.W., Zeng, Y., Zang, C.A.: Supersonic flutter analysis based on a local piston theory. AIAA J. 47(10), 2321–2328 (2009). https://doi.org/10.2514/1.37750
Oh, I.K., Kim, D.H.: Vibration characteristics and supersonic flutter of cylindrical composite panels with large thermoelastic deflections. Compos. Struct. 90(2), 208–216 (2009). https://doi.org/10.1016/j.compstruct.2009.03.012
Haddadpour, H., Navazi, H., Shadmehri, F.: Nonlinear oscillations of a fluttering functionally graded plate. Compos. Struct. 79(2), 242–250 (2007). https://doi.org/10.1016/j.compstruct.2006.01.006
Chorfi, S., Houmat, A.: Nonlinear free vibration of a moderately thick doubly curved shallow shell of elliptical plan-form. Int. J. Comput. Methods 6(04), 615–632 (2009). https://doi.org/10.1142/S0219876209002030
Hosseini, M., Fazelzadeh, S.: Aerothermoelastic post-critical and vibration analysis of temperature-dependent functionally graded panels. J. Therm. Stresses 33(12), 1188–1212 (2010). https://doi.org/10.1080/01495739.2010.510754
Kiani, Y., Shakeri, M., Eslami, M.: Thermoelastic free vibration and dynamic behaviour of an FGM doubly curved panel via the analytical hybrid Laplace-Fourier transformation. Acta Mech. 223(6), 1199–1218 (2012). https://doi.org/10.1007/s00707-012-0629-9
Li, F.M., Song, Z.G.: Aeroelastic flutter analysis for 2D Kirchhoff and Mindlin panels with different boundary conditions in supersonic airflow. Acta Mech. 225(12), 3339–3351 (2014). https://doi.org/10.1007/s00707-014-1141-1
Shen, H.S., Chen, X., Guo, L., Wu, L., Huang, X.L.: Nonlinear vibration of FGM doubly curved panels resting on elastic foundations in thermal environments. Aerosp. Sci. Technol. 47, 434–446 (2015). https://doi.org/10.1016/j.ast.2015.10.011
Wattanasakulpong, N., Chaikittiratana, A.: An analytical investigation on free vibration of FGM doubly curved shallow shells with stiffeners under thermal environment. Aerosp. Sci. Technol. 40, 181–190 (2015). https://doi.org/10.1016/j.ast.2013.12.002
Ganji, H.F., Dowell, E.H.: Panel flutter prediction in two-dimensional flow with enhanced piston theory. J. Fluids Struct. 63, 97–102 (2016). https://doi.org/10.1016/j.jfluidstructs.2016.03.003
Grover, N., Singh, B., Maiti, D.: An inverse trigonometric shear deformation theory for supersonic flutter characteristics of multilayered composite plates. Aerosp. Sci. Technol. 52, 41–51 (2016). https://doi.org/10.1016/j.ast.2016.02.017
MalekzadehFard, K., Shokrollahi, S.: Higher order flutter analysis of doubly curved sandwich panels with variable thickness under aerothermoelastic loading. Struct. Eng. Mech. 60(1), 1–19 (2016). https://doi.org/10.12989/sem.2016.60.1.001
Sankar, A., Natarajan, S., Ben Zine, T., Ganapathi, M.: Investigation of supersonic flutter of thick doubly curved sandwich panels with CNT reinforced face sheets using higher-order structural theory. Compos. Struct. 127, 340–355 (2015). https://doi.org/10.1016/j.compstruct.2015.02.047
Song, M., Kitipornchai, S., Yang, J.: Free and forced vibrations of functionally graded polymer composite plates reinforced with graphene nanoplatelets. Compos. Struct. 159, 579–588 (2017). https://doi.org/10.1016/j.compstruct.2016.09.070
Zare Jouneghani, F., Dimitri, R., Bacciocchi, M., Tornabene, F.: Free vibration analysis of functionally graded porous doubly-curved shells based on the first-order shear deformation theory. Appl. Sci. 7(12), 1252 (2017). https://doi.org/10.3390/app7121252
Rezaei, A.S., Saidi, A.R., Abrishamdari, M., PourMohammadi, M.H.: Natural frequencies of functionally graded plates with porosities via a simple four variable plate theory: an analytical approach. Thin-Walled Struct. 120, 366–377 (2017). https://doi.org/10.1016/j.tws.2017.08.003
Pouresmaeeli, S., Fazelzadeh, S.A., Ghavanloo, E., Marzocca, P.: Uncertainty propagation in vibrational characteristics of functionally graded carbon nanotube-reinforced composite shell panels. Int. J. Mech. Sci. 149, 549–558 (2018). https://doi.org/10.1016/j.ijmecsci.2017.05.049
Lei, Z.X., Zhang, L.W., Liew, K.M., Yu, J.L.: Dynamic stability analysis of carbon nanotube-reinforced functionally graded cylindrical panels using the element-free KP-Ritz method. Compos. Struct. 113, 328–338 (2014). https://doi.org/10.1016/j.compstruct.2014.03.035
Shahverdi, H., Khalafi, V., Noori, S.: Aerothermoelastic analysis of functionally graded plates using generalized differential quadrature method. Lat. Am. J. Solids Struct. 13(4), 796–818 (2016). https://doi.org/10.1590/1679-78252072
Navazi, H., Haddadpour, H.: Aero-thermoelastic stability of functionally graded plates. Compos. Struct. 80(4), 580–587 (2007). https://doi.org/10.1016/j.compstruct.2006.07.014
Kiani, Y.: Free vibration of FG-CNT reinforced composite spherical shell panels using Gram–Schmidt shape functions. Compos. Struct. 159, 368–381 (2017). https://doi.org/10.1016/j.compstruct.2016.09.079
Mehar, K., Panda, S.K., Patle, B.K.: Thermoelastic vibration and flexural behaviour of FG-CNT reinforced composite curved panel. Int. J. Appl. Mech. 9(04), 1750046 (2017). https://doi.org/10.1142/S1758825117500466
Zhou, J., Xu, M., Yang, Z.: Aeroelastic stability analysis of curved composite panels with embedded Macro Fiber Composite actuators. Compos. Struct. 208, 725–734 (2019). https://doi.org/10.1016/j.compstruct.2018.10.035
Lin, H., Cao, D., Xu, Y.: Vibration, buckling and aeroelastic analyses of functionally graded multilayer graphene-nanoplatelets-reinforced composite plates embedded in piezoelectric layers. Int. J. Appl. Mech. 10(03), 1850023 (2018). https://doi.org/10.1142/S1758825118500230
Saidi, A.R., Bahaadini, R., Majidi-Mozafari, K.: On vibration and stability analysis of porous plates reinforced by graphene platelets under aerodynamical loading. Compos. B Eng. 164, 778–799 (2019). https://doi.org/10.1016/j.compositesb.2019.01.074
Bahaadini, R., Saidi, A.R., Majidi-Mozafari, K.: Aeroelastic flutter analysis of thick porous plates in supersonic flow. Int. J. Appl. Mech. 11(10), 1950096 (2019). https://doi.org/10.1142/S1758825119500960
Muc, A., Flis, J., Augustyn, M.: Optimal design of plated/shell structures under flutter constraints—a literature review. Materials 12(24), 4215 (2019). https://doi.org/10.3390/ma12244215
Arani, A.G., Kiani, F., Afshari, H.: Aeroelastic analysis of laminated FG-CNTRC cylindrical panels under yawed supersonic flow. Int. J. Appl. Mech. 11(06), 1950052 (2019). https://doi.org/10.1142/S1758825119500522
Aditya, S., Haboussi, M., Shubhendu, S., Ganapathi, M., Polit, O.: Supersonic flutter study of porous 2D curved panels reinforced with graphene platelets using an accurate shear deformable finite element procedure. Compos. Struct. 241, 112058 (2020). https://doi.org/10.1016/j.compstruct.(2020).112058
Bahaadini, R., Saidi, A.R., Hosseini, M.: Dynamic stability of fluid-conveying thin-walled rotating pipes reinforced with functionally graded carbon nanotubes. Acta Mech. 229, 5013–5029 (2018). https://doi.org/10.1007/s00707-018-2286-0
Majidi, M.H., Azadi, M., Fahham, H.: Effect of CNT reinforcements on the flutter boundaries of cantilever trapezoidal plates under yawed supersonic fluid flow. Mech. Based Des. Struct. Mach. (2020). https://doi.org/10.1080/15397734.2020.1723107
Esmaeili, H., Kiani, Y., Beni, Y.T.: Vibration characteristics of composite doubly curved shells reinforced with graphene platelets with arbitrary edge supports. Acta Mech. (2022). https://doi.org/10.1007/s00707-021-03140-z
An, X.M., Sun, W.: Study of aeroelastic response of cylindrical composite panels in A high-speed flow. Int. J. Modern Phys. B 34(14n16), 2040116 (2020). https://doi.org/10.1142/S0217979220401165
Ye, L., Ye, Z., Ye, K., Wu, J.: Aeroelastic stability and nonlinear flutter analysis of viscoelastic heated panel in shock-dominated flows. Aerosp. Sci. Technol. 117, 106909 (2021). https://doi.org/10.1016/j.ast.2021.106909
Rahmanian, M., Javadi, M.: Supersonic aeroelasticity and dynamic instability of functionally graded porous cylindrical shells using a unified solution formulation. Int. J. Struct. Stab. Dyn. 20(12), 2050132 (2020). https://doi.org/10.1142/S0219455420501321
Adamian, A., Hosseini Safari, K., Sheikholeslami, M., Habibi, M., Alforjan, M.S.H., Chen, G.: Critical temperature and frequency characteristics of GPLs-reinforced composite doubly curved panel. Appl. Sci. 10(9), 3251 (2020). https://doi.org/10.3390/app10093251
Zhou, X., Wang, Y., Zhang, W.: Vibration and flutter characteristics of GPL-reinforced functionally graded porous cylindrical panels subjected to supersonic flow. Acta Astronaut. 183, 89–100 (2021). https://doi.org/10.1016/j.actaastro.2021.03.003
AminYazdi, A.: Flutter of geometrical imperfect functionally graded carbon nanotubes doubly curved shells. Thin-Walled Struct. 164, 107798 (2021). https://doi.org/10.1016/j.tws.2021.107798
Subramani, M., Subramani, M., Ramamoorthy, M., Arumugam, A.B., Selvaraj, R.: Free and forced vibration characteristics of CNT reinforced composite spherical sandwich shell panels with MR elastomer core. Int. J. Struct. Stab. Dyn. 21(10), 2150136 (2021). https://doi.org/10.1142/S0219455421501364
Majidi Mozafari, K., Bahaadini, R., Saidi, A.R.: Aeroelastic flutter analysis of functionally graded spinning cylindrical shells reinforced with graphene nanoplatelets in supersonic flow. Mater. Res. Express 8(11), 115012 (2021). https://doi.org/10.1088/2053-1591/ac2ce4
Abdollahi, M., Saidi, A.R., Bahaadini, R.: Aeroelastic analysis of symmetric and non-symmetric trapezoidal honeycomb sandwich plates with FG porous face sheets. Aerosp. Sci. Technol. 119, 107211 (2021). https://doi.org/10.1016/j.ast.2021.107211
Merdaci, S., Adda, H.M., Hakima, B., Dimitri, R., Tornabene, F.: Higher-order free vibration analysis of porous functionally graded plates. J. Compos. Sci. 5(11), 305 (2021). https://doi.org/10.3390/jcs5110305
Houshangi, A., Jafari, A.A., Haghighi, S.E., Nezami, M.: Supersonic flutter characteristics of truncated sandwich conical shells with MR core. Thin-Walled Struct. 173, 108888 (2022). https://doi.org/10.1016/j.tws.2022.108888
Chen, J., Han, R., Liu, D., Zhang, W.: Active flutter suppression and aeroelastic response of functionally graded multilayer graphene nanoplatelet reinforced plates with piezoelectric patch. Appl. Sci. 12(3), 1244 (2022). https://doi.org/10.3390/app12031244
Arani, A.G., Eskandari, M., Haghparast, E.: The supersonic flutter behavior of sandwich plates with a magnetorheological elastomer core and GNP-reinforced face sheets. Int. J. Appl. Mech. (2022). https://doi.org/10.1142/S1758825122500156
Khorshidi, K., Karimi, M., Amabili, M.: Aeroelastic analysis of rectangular plates coupled to sloshing fluid. Acta Mech. 231, 3183–3198 (2020). https://doi.org/10.1007/s00707-020-02696-6
Crawley, E.F., De Luis, J.: Use of piezoelectric actuators as elements of intelligent structures. AIAA J. 25(10), 1373–1385 (1987). https://doi.org/10.2514/3.9792
Zhou, R.C., Lai, Z., Xue, D.Y., Huang, J.K., Mei, C.: Suppression of nonlinear panel flutter with piezoelectric actuators using finite element method. AIAA J. 33(6), 1098–1105 (1995). https://doi.org/10.2514/3.12530
Song, Z.G., Li, F.M.: Active aeroelastic flutter analysis and vibration control of supersonic composite laminated plate. Compos. Struct. 94(2), 702–713 (2012). https://doi.org/10.1016/j.compstruct.2011.09.005
Li, F.M.: Active aeroelastic flutter suppression of a supersonic plate with piezoelectric material. Int. J. Eng. Sci. 51, 190–203 (2012). https://doi.org/10.1016/j.ijengsci.2011.10.003
Tsushima, N., Su, W.: Flutter suppression for highly flexible wings using passive and active piezoelectric effects. Aerosp. Sci. Technol. 65, 78–89 (2017). https://doi.org/10.1016/j.ast.2017.02.013
Li, F.M., Chen, Z.B., Cao, D.Q.: Improving the aeroelastic flutter characteristics of supersonic beams using piezoelectric material. J. Intell. Mater. Syst. Struct. 22(7), 615–629 (2011). https://doi.org/10.1177/1045389X11403820
Xue, Y., Li, J., Li, F., Song, Z.: Flutter and thermal buckling properties and active control of functionally graded piezoelectric material plate in supersonic airflow. Acta Mech. Solida Sin. 33(5), 692–706 (2020). https://doi.org/10.1007/s10338-020-00159-y
Wang, Q., Quek, S.T., Sun, C.T., Liu, X.: Analysis of piezoelectric coupled circular plate. Smart Mater. Struct. 10(2), 229 (2001). https://doi.org/10.1088/0964-1726/10/2/308
Farsangi, M.A., Saidi, A.: Levy type solution for free vibration analysis of functionally graded rectangular plates with piezoelectric layers. Smart Mater. Struct. 21(9), 094017 (2012). https://doi.org/10.1088/0964-1726/21/9/094017
Almeida, A., Donadon, M.V., De Faria, A.R., Almeida, S.F.M.: The effect of piezoelectrically induced stress stiffening on the aeroelastic stability of curved composite panels. Compos. Struct. 94(12), 3601–3611 (2012). https://doi.org/10.1016/j.compstruct.2012.06.008
Zhang, L., Song, Z., Liew, K.: Computation of aerothermoelastic properties and active flutter control of CNT reinforced functionally graded composite panels in supersonic airflow. Comput. Methods Appl. Mech. Eng. 300, 427–441 (2016). https://doi.org/10.1016/j.cma.2015.11.029
Tian, W., Zhao, T., Yang, Z.: Nonlinear electro-thermo-mechanical dynamic behaviours of a supersonic functionally graded piezoelectric plate with general boundary conditions. Compos. Struct. 261, 113326 (2021). https://doi.org/10.1016/j.compstruct.2020.113326
Tham, V., Tran, H., Tu, T.: Vibration characteristics of piezoelectric functionally graded carbon nanotube-reinforced composite doubly-curved shells. Appl. Math. Mech. 42(6), 819–840 (2021). https://doi.org/10.1007/s10483-021-2730-7
Reddy, J.N.: Mechanics of Laminated Composite Plates and Shells: Theory and Analysis. CRC Press, Boca Raton (2004)
Ebrahimi, F., Jafari, A.: A higher-order thermomechanical vibration analysis of temperature-dependent FGM beams with porosities. J. Eng. (2016). https://doi.org/10.1155/2016/9561504
Dowell, E.H.: Aeroelasticity of Plates and Shells, vol. 1. Springer Science & Business Media, Berlin (1974)
Wattanasakulpong, N., Ungbhakorn, V.: Linear and nonlinear vibration analysis of elastically restrained ends FGM beams with porosities. Aerosp. Sci. Technol. 32(1), 111–120 (2014). https://doi.org/10.1016/j.ast.2013.12.002
Farsangi, M.A., Saidi, A.R., Batra, R.C.: Analytical solution for free vibrations of moderately thick hybrid piezoelectric laminated plates. J. Sound Vib. 332(22), 5981–5998 (2013). https://doi.org/10.1016/j.jsv.2013.05.010
Murakami, H.: Laminated composite plate theory with improved in-plane responses. J. Appl. Mech. 53(1), 661–666 (1986)
Sciuva, D.M.: An improved shear-deformation theory for moderately thick multilayered anisotropic shells and plates. J. Appl. Mech. 54(1), 589–596 (1987)
Matsunaga, H.: Free vibration and stability of functionally graded shallow shells according to a 2D higher-order deformation theory. Compos. Struct. 84(2), 132–146 (2008). https://doi.org/10.1016/j.compstruct.2007.07.006
Akbari, H., Azadi, M., Fahham, H.: Flutter prediction of cylindrical sandwich panels with saturated porous core under supersonic yawed flow. Proc. Inst. Mech. Eng. C J. Mech. Eng. Sci. 235(16), 2968–2984 (2021). https://doi.org/10.1177/0954406220960786
Prakash, T., Ganapathi, M.: Supersonic flutter characteristics of functionally graded flat panels including thermal effects. Compos. Struct. 72(1), 10–18 (2006). https://doi.org/10.1016/j.compstruct.2004.10.007
Fung, Y.: On two-dimensional panel flutter. J. Aerosp. Sci. 25(3), 145–160 (1958). https://doi.org/10.2514/8.7557
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Appendices
Appendix A
In Eq. (20), the terms expressing inertia and the resulting forces and moments are expressed as follows:
The stiffness coefficients are presented in Eq. (21) as follows:
The constant quantities in Eq. (22), can be expressed as follow:
For open-circuit condition:
and for closed-circuit condition:
Appendix B
In Eq. (26), the definitions of constant quantities are expressed as follows:
For open-circuit condition:
and for closed-circuit condition:
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Abbaslou, M., Saidi, A.R. & Bahaadini, R. Vibration and dynamic instability analyses of functionally graded porous doubly curved panels with piezoelectric layers in supersonic airflow. Acta Mech 234, 6131–6167 (2023). https://doi.org/10.1007/s00707-023-03699-9
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DOI: https://doi.org/10.1007/s00707-023-03699-9