Nonlinear analysis of functionally graded skewed and tapered wing-like plates including porosities: A bifurcation study
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Tarih
2021
Dergi Başlığı
Dergi ISSN
Cilt Başlığı
Yayıncı
Elsevier Sci Ltd
Erişim Hakkı
info:eu-repo/semantics/closedAccess
Özet
In the present study, nonlinear panel flutter and bifurcation behavior of functionally graded ceramic/metal winglike tapered and skewed plates are investigated. Porosities are distributed over the cross-section of the functionally graded structure. The flutter speed, limit cycle oscillations, and bifurcation diagrams of the functionally graded plate with two types of geometrical non-uniformities being skewness and taperness are explored. Nonlinear structural model is utilized based on the virtual work principle by including the von-Karman nonlinear kinematic strain assumption. The first order shear deformation theory is employed to consider the transverse shear effect in the structural model. First-order linear piston theory is used to model the aerodynamic loading while the generalized differential quadrature method is employed to solve the governing equations of motion. Time integration of the final ordinary equations of motion is carried out using the Newmark average acceleration method. Different volume fractions are investigated to enhance the flutter instability margins and post-flutter behavior of functionally graded plates. Results demonstrate that the volume fraction and porosity coefficients have significant effects on dynamic behavior and limit cycle oscillation amplitudes.
Açıklama
Anahtar Kelimeler
Functionally graded material (FGM), Nonlinear aeroelasticity, Limit cycle oscillation (LCO), Tapered plates, Skewed plates, Porosity, Generalized differential quadrature (GDQ)
Kaynak
Thin-Walled Structures
WoS Q Değeri
Q1
Scopus Q Değeri
Q1
Cilt
160
