Journal ArticleDOI
Panel flutter - A review of the aeroelastic stability of plates and shells
TLDR
In this article, panel flutter theory applied to aeroelastic stability of flat unloaded plates and cylindrical shells is applied to the stability of aero-elastic vehicles.Abstract:
Panel flutter theory applied to aeroelastic stability of flat unloaded plates and cylindrical shellsread more
Citations
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Journal ArticleDOI
On the use of higher-order finite-difference schemes on curvilinear and deforming meshes
Miguel R. Visbal,Datta Gaitonde +1 more
TL;DR: A simple technique is adopted which ensures metric cancellation and thus ensures freestream preservation even on highly distorted curvilinear meshes, and metric cancellation is guaranteed regardless of the manner in which grid speeds are defined.
Book
Nonlinear Vibrations and Stability of Shells and Plates
TL;DR: In this article, a comparison of different shell theories for nonlinear vibrations and stability of circular cylindrical shells is presented. But the authors do not consider the effect of boundary conditions on the large-amplitude vibrations of circular cylinders.
Journal ArticleDOI
Review of studies on geometrically nonlinear vibrations and dynamics of circular cylindrical shells and panels, with and without fluid-structure interaction
Journal ArticleDOI
Studies on Fluid-Thermal-Structural Coupling for Aerothermoelasticity in Hypersonic Flow
Adam J. Culler,Jack J. McNamara +1 more
TL;DR: In this paper, the tradeoff between computational cost and accuracy is evaluated for aerothermoelastic analysis based on either quasi-static or time-averaged dynamic fluid-thermal-structural coupling, as well as computational fluid dynamics based reduced-order modeling of the aerodynamic heat flux.
Journal ArticleDOI
Finite element nonlinear panel flutter with arbitrary temperatures in supersonic flow
David Y. Xue,Chuh Mei +1 more
TL;DR: In this paper, a finite element frequency domain method for predicting nonlinear flutter response of panels with temperature effects is presented, using the principle of virtual work, the element nonlinear stiffness formulation for a panel under a combined thermal and aerodynamic loads is derived on the bases of von Karman's large deflection plate theory, the first-order piston theory aerodynamics and the quasi-steady thermal stress theory.
References
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Journal ArticleDOI
Nonlinear oscillations of a fluttering plate. II.
TL;DR: Quasi-steady aerodynamic and von Karman large deflection plate theory equations of nonlinear oscillations of fluttering plate for single mode subsonic and sonic or coupled mode supersonic oscillations are given in this article.
Journal ArticleDOI
Theoretical considerations of panel flutter at high supersonic Mach numbers.
TL;DR: In this paper, the general characteristics of panel flutter at high supersonic Mach numbers are examined theoretically using linear plate theory and two-dimensional first-order aerodynamics, and the important role of damping, the relationship between traveling and standing wave theories of panels flutter and the effects of edge conditions.