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Nonlinear analysis of functionally graded skewed and tapered wing-like plates including porosities: A bifurcation study
https://orcid.org/0000-0002-2552-8616
Abstract In the present study, nonlinear panel flutter and bifurcation behavior of functionally graded ceramic/metal wing-like 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.
Highlights Results demonstrate that the volume fraction and porosity coefficient have significant effects on the dynamic behavior and LCOs of the FG plates. LCO characteristics of FG ceramic/metal and porous plates in supersonic flow are determined by bifurcation diagrams. Three volume fraction exponents of FG plate along with two types of porosity distributions are studied to investigate the subcritical and supercritical behaviors for the FG cantilevered plates. This is the first bifurcation analysis of functionally graded wing-like plates with complex geometries, skewback angles, taper ratio in conjunction with two porosity distributions. It is the first time that the effect of porosity is investigated on the post flutter behavior of the FG plates using bifurcation diagrams. All previous studies of FG porous plates are focused on the linear aeroelastic analysis.
Nonlinear analysis of functionally graded skewed and tapered wing-like plates including porosities: A bifurcation study
https://orcid.org/0000-0002-2552-8616
Abstract In the present study, nonlinear panel flutter and bifurcation behavior of functionally graded ceramic/metal wing-like 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.
Highlights Results demonstrate that the volume fraction and porosity coefficient have significant effects on the dynamic behavior and LCOs of the FG plates. LCO characteristics of FG ceramic/metal and porous plates in supersonic flow are determined by bifurcation diagrams. Three volume fraction exponents of FG plate along with two types of porosity distributions are studied to investigate the subcritical and supercritical behaviors for the FG cantilevered plates. This is the first bifurcation analysis of functionally graded wing-like plates with complex geometries, skewback angles, taper ratio in conjunction with two porosity distributions. It is the first time that the effect of porosity is investigated on the post flutter behavior of the FG plates using bifurcation diagrams. All previous studies of FG porous plates are focused on the linear aeroelastic analysis.
Nonlinear analysis of functionally graded skewed and tapered wing-like plates including porosities: A bifurcation study
https://orcid.org/0000-0002-2552-8616
Abstract In the present study, nonlinear panel flutter and bifurcation behavior of functionally graded ceramic/metal wing-like 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.
Highlights Results demonstrate that the volume fraction and porosity coefficient have significant effects on the dynamic behavior and LCOs of the FG plates. LCO characteristics of FG ceramic/metal and porous plates in supersonic flow are determined by bifurcation diagrams. Three volume fraction exponents of FG plate along with two types of porosity distributions are studied to investigate the subcritical and supercritical behaviors for the FG cantilevered plates. This is the first bifurcation analysis of functionally graded wing-like plates with complex geometries, skewback angles, taper ratio in conjunction with two porosity distributions. It is the first time that the effect of porosity is investigated on the post flutter behavior of the FG plates using bifurcation diagrams. All previous studies of FG porous plates are focused on the linear aeroelastic analysis.
Nonlinear analysis of functionally graded skewed and tapered wing-like plates including porosities: A bifurcation study
Farsadi, Touraj (author) / Rahmanian, Mohammad (author) / Kurtaran, Hasan (author)
Thin-Walled Structures ; 160
2020-11-28
Article (Journal)
Electronic Resource
English
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