Journal ArticleDOI
Nonlinear flutter of aerothermally buckled composite shells with damping treatments
Won-Ho Shin,Il-Kwon Oh,In Lee +2 more
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TLDR
In this paper, the aerothermally buckled cylindrical composite shells with various damping treatments were implemented using the theory of layerwise displacement field, and the arc-length method and iterative nonlinear scheme were taken up to estimate the postbuckling deformation of composite shells due to aerothermal loads.About:
This article is published in Journal of Sound and Vibration.The article was published on 2009-07-24. It has received 26 citations till now. The article focuses on the topics: Flutter & Vibration.read more
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Journal ArticleDOI
Recent research advances on the dynamic analysis of composite shells: 2000-2009
TL;DR: A review of the state-of-the-art in the area of dynamic analysis of composite shells can be found in this article, where the main aim is to provide a broad perspective of the current state of the art in this field.
Journal ArticleDOI
Non-linear vibrations of shells: A literature review from 2003 to 2013
Farbod Alijani,Marco Amabili +1 more
TL;DR: In this paper, a review of geometrically non-linear free and forced vibrations of shells made of traditional and advanced materials is presented, including closed shells and curved panels made of isotropic, laminated composite, piezoelectric, functionally graded and hyperelastic materials.
Journal ArticleDOI
Active aeroelastic flutter analysis and vibration control of supersonic composite laminated plate
Zhi-Guang Song,Feng-Ming Li +1 more
TL;DR: In this paper, the active aeroelastic flutter analysis and vibration control at the flutter bounds of the supersonic composite laminated plates with the piezoelectric patches are studied.
Journal ArticleDOI
Review of Recent Literature on Static Analyses of Composite Shells: 2000-2010
TL;DR: In this article, a review of the static analysis of composite shells is presented, with an emphasis on the analysis performed (static, buckling, postbuckling, and others), complicating effects in both material (e.g. piezoelectric) and structure (i.e. stiffened shells), and various shell geometries (cylindrical, conical, spherical and others).
Journal ArticleDOI
Active aeroelastic flutter suppression of a supersonic plate with piezoelectric material
TL;DR: In this paper, the authors investigated the active aeroelastic flutter properties of supersonic plates by using the piezoelectric material and found that the active stiffness and active mass have prominent effects on the flutter characteristics of the su personic plates.
References
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Journal ArticleDOI
Panel flutter - A review of the aeroelastic stability of plates and shells
TL;DR: 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.
Book
Elastostatics and Kinetics of Anisotropic and Heterogeneous Shell-Type Structures
Liviu Librescu,J. G. Simmonds +1 more
TL;DR: The anvatquynhon.xyz project as discussed by the authors is a high quality resource for free books books, including classics and out-of-print books, which is compatible for Kindles, Nooks, iPads and most e-readers.
Journal ArticleDOI
Flutter of a buckled plate as an example of chaotic motion of a deterministic autonomous system
TL;DR: In this paper, the equations of motion for aeroelasticity of plates and shells are well established and results obtained by numerical time integration have been compared to those obtained by topological theories of dynamics and also from experiment.
Journal ArticleDOI
Thermal post-buckling and flutter characteristics of composite plates embedded with shape memory alloy fibers
TL;DR: In this article, the effect of shape memory alloy (SMA) fibers on the critical temperature, thermal postbuckling deflection, natural frequency and critical dynamic pressure of the SMA composite plate was investigated.
Journal ArticleDOI
Flutter and Buckling of General Laminated Plates
TL;DR: In this article, an anisotropic buckling and flutter analysis with allowance for both bending-extensional coupling and bending-twisting coupling within the framework of linear small deflection theory for simply supported general laminated plates is developed with particular emphasis on assessing the range of applicability of classical orthotropic plate theory.
Related Papers (5)
Effects of hysteretic and aerodynamic damping on supersonic panel flutter of composite plates
Kyo-Nam Koo,Woo-Seok Hwang +1 more