Flutter analysis of multi-directional functionally graded sector poroelastic disks
For the first time, in this article, stable/unstable zones of multi-directional functionally graded
(MD-FG) sector disks under aerodynamic pressures are sought. Also, because of porous …
(MD-FG) sector disks under aerodynamic pressures are sought. Also, because of porous …
Nonlinear supersonic flutter for the viscoelastic orthotropic cylindrical shells in supersonic flow
BA Khudayarov, FZ Turaev - Aerospace Science and Technology, 2019 - Elsevier
On the example of an orthotropic shell, the problems of the dynamics of thin-walled
structures under aerodynamic loading are studied, taking into account the viscoelastic …
structures under aerodynamic loading are studied, taking into account the viscoelastic …
Flutter and thermal buckling control for composite laminated panels in supersonic flow
FM Li, ZG Song - Journal of Sound and Vibration, 2013 - Elsevier
Aerothermoelastic analysis for composite laminated panels in supersonic flow is carried out.
The flutter and thermal buckling control for the panels are also investigated. In the modeling …
The flutter and thermal buckling control for the panels are also investigated. In the modeling …
Methods of continuation and their implementation in the COCO software platform with application to delay differential equations
This paper treats comprehensively the construction of problems from nonlinear dynamics
and constrained optimization amenable to parameter continuation techniques and with …
and constrained optimization amenable to parameter continuation techniques and with …
Active aerothermoelastic flutter suppression of composite laminated panels with time-dependent boundaries
Aerothermoelastic characteristics of composite laminated panels with time-dependent
boundary conditions are investigated. The macro fiber composite (MFC) which is more …
boundary conditions are investigated. The macro fiber composite (MFC) which is more …
Nonlinear thermal flutter analysis of variable angle tow composite curved panels in supersonic airflow
X Chen, G Nie - Composite Structures, 2021 - Elsevier
Abstract The advanced Automated Fibre Placement (AFP) technologies make the synthesis
of Variable Angle Tow (VAT) composites possible, which provides an extended space for the …
of Variable Angle Tow (VAT) composites possible, which provides an extended space for the …
Nonlinear flutter response of a composite plate applying curvilinear fiber paths
In the present study, nonlinear flutter and post-flutter behavior of a variable stiffness
composite wing-like plate is investigated. The variable stiffness is obtained by varying fiber …
composite wing-like plate is investigated. The variable stiffness is obtained by varying fiber …
Nonlinear viscoelastic heated panel flutter with aerodynamic loading exerted on both surfaces
X Wang, Z Yang, W Wang, W Tian - Journal of Sound and Vibration, 2017 - Elsevier
A nonlinear flutter analysis of viscoelastic heated panels with aerodynamic loading exerting
on its both surfaces is presented. The aeroelastic motion equations of such panels can be …
on its both surfaces is presented. The aeroelastic motion equations of such panels can be …
Aeroelastic flutter analysis of thick porous plates in supersonic flow
The aeroelastic flutter analysis of thick porous plates surrounded with piezoelectric layers in
supersonic flow is studied. In order to aeroelastic analysis of the thick porous-cellular plate …
supersonic flow is studied. In order to aeroelastic analysis of the thick porous-cellular plate …
Aeroelastic analysis of pre-stressed variable stiffness composite panels
The effect of in-plane stresses on the stability behaviors of constant stiffness and variable
stiffness composite panels, exposed to aerodynamic pressure, is studied using the finite …
stiffness composite panels, exposed to aerodynamic pressure, is studied using the finite …