A new method for suppressing nonlinear flutter and thermal buckling of composite lattice sandwich beams
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Publication:2115390
DOI10.1007/S00707-021-03107-0OpenAlexW4206131411MaRDI QIDQ2115390
Publication date: 15 March 2022
Published in: Acta Mechanica (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1007/s00707-021-03107-0
Thin bodies, structures (74Kxx) Dynamical problems in solid mechanics (74Hxx) Coupling of solid mechanics with other effects (74Fxx)
Related Items (1)
Cites Work
- Flutter stabilization of cantilevered plates using a bonded patch
- On the nonlinear dynamic responses of FG-CNTRC beams exposed to aerothermal loads using third-order piston theory
- Analytical modeling and finite element simulation of the plastic collapse of sandwich beams with pin-reinforced foam cores
- Coherent structures and their influence on the dynamics of aeroelastic panels
- Nonlinear aero-thermal flutter postponement of supersonic laminated composite beams with shape memory alloys
- Vibro-acoustic response of sandwich plates with functionally graded core
- Aeroelastic analysis of rectangular plates coupled to sloshing fluid
- Nonlinear primary resonances of lattice sandwich beams with pyramidal truss core and viscoelastic surfaces
- Parametric and internal resonance of a transporting plate with a varying tension
- Aeroelastic analysis and active flutter control of nonlinear lattice sandwich beams
- The Nonlinear Dynamical Analysis of a Sandwich Plate with In-Plane Loading in Supersonic Flow
- Multimode Approach to Nonlinear Supersonic Flutter of Imperfect Circular Cylindrical Shells
- Discrete element approach to flutter of skew panels with in-plane forces under yawed supersonic flow
- Free vibration of curved sandwich beams by the method of finite elements
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