Flutter characteristics and free vibrations of rectangular functionally graded porous plates

被引:24
作者
Muc, Aleksander [1 ]
Flis, Justyna [1 ]
机构
[1] Cracow Univ Technol, Inst Machine Design, PL-31155 Krakow, Poland
关键词
Supersonic flutter characteristics; Free vibrations; Porous functionally graded material; Rectangular plates; Analytical methods; Classical and first order transverse shear deformation theory; SHEAR DEFORMATION-THEORY; SUPERSONIC FLUTTER; BUCKLING ANALYSIS; THERMOELASTIC STABILITY; SANDWICH PANELS; OPTIMAL-DESIGN; GRADIENT;
D O I
10.1016/j.compstruct.2020.113301
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
This paper investigates the flutter characteristics and free vibrations of porous functionally graded plates using the analytical and Rayleigh-Ritz methods. The analytical methods can be employed for the solution of six of 21 arbitrary boundary conditions (the combinations of clamped, simply supported and free). The influence of five various models of porosity is studied, including different variations of stiffness/density along the thickness and/or length of a plate. The analysis is carried out for the classical (CPT) and first order transverse shear deformation (FSDT) theory. For CPT analytical solutions the effects of porosity are characterized by two simple correction factors that shows a very good agreement with the numerical Rayleigh-Ritz method. Parametric studies illustrate the possibility of increasing natural frequencies as well as flutter critical aerodynamic pressures and the necessity of implementing the optimization techniques to find the best solutions from the engineering point of view. The solutions are valid for thin and moderately thick porous FGM plates although the proposed methodology of computations can be easily adopted to the application of different approximations of 2D displacement distributions (see Appendix).
引用
收藏
页数:11
相关论文
共 70 条
  • [1] Dynamic stability of sandwich functionally graded micro-beam based on the nonlocal strain gradient theory with thermal effect
    Al-shujairi, Mohammed
    Mollamahmutoglu, Cagri
    [J]. COMPOSITE STRUCTURES, 2018, 201 : 1018 - 1030
  • [2] Analysis of functionally graded stiffened plates based on FSDT utilizing reproducing kernel particle method
    Ardestani, M. Memar
    Soltani, B.
    Shams, Sh.
    [J]. COMPOSITE STRUCTURES, 2014, 112 : 231 - 240
  • [3] Accurate solution for free vibration analysis of functionally graded thick rectangular plates resting on elastic foundation
    Baferani, A. Hasani
    Saidi, A. R.
    Ehteshami, H.
    [J]. COMPOSITE STRUCTURES, 2011, 93 (07) : 1842 - 1853
  • [4] Aerothermoelastic flutter analysis of pre-twisted thin-walled rotating blades reinforced with functionally graded carbon nanotubes
    Bahaadini, Reza
    Saidi, Ali Reza
    [J]. EUROPEAN JOURNAL OF MECHANICS A-SOLIDS, 2019, 75 : 285 - 306
  • [5] An efficient and simple higher order shear and normal deformation theory for functionally graded material (FGM) plates
    Belabed, Zakaria
    Houari, Mohammed Sid Ahmed
    Tounsi, Abdelouahed
    Mahmoud, S. R.
    Beg, O. Anwar
    [J]. COMPOSITES PART B-ENGINEERING, 2014, 60 : 274 - 283
  • [6] Modeling and analysis of functionally graded materials and structures
    Birman, Victor
    Byrd, Larry W.
    [J]. APPLIED MECHANICS REVIEWS, 2007, 60 (1-6) : 195 - 216
  • [7] Levy-type solution for buckling analysis of thick functionally graded rectangular plates based on the higher-order shear deformation plate theory
    Bodaghi, M.
    Saidi, A. R.
    [J]. APPLIED MATHEMATICAL MODELLING, 2010, 34 (11) : 3659 - 3673
  • [8] Bolotin VV, 1961, NONCONSERVATIVE PROB
  • [9] Thermoelastic stability analysis of functionally graded plates: An analytical approach
    Bouazza, M.
    Tounsi, A.
    Adda-Bedia, E. A.
    Megueni, A.
    [J]. COMPUTATIONAL MATERIALS SCIENCE, 2010, 49 (04) : 865 - 870
  • [10] Investigations on the influences of elastic foundations on the aerothermoelastic flutter and thermal buckling properties of lattice sandwich panels in supersonic airflow
    Chai, Yu-Yang
    Song, Zhi-Guang
    Li, Feng-Ming
    [J]. ACTA ASTRONAUTICA, 2017, 140 : 176 - 189