Optimal locations of magnetorheological fluid pockets embedded in an elastically supported honeycomb sandwich beams for supersonic flutter suppression
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Publication:1713670
DOI10.1016/J.EUROMECHSOL.2018.11.003zbMath1406.74203OpenAlexW2900188583WikidataQ128971964 ScholiaQ128971964MaRDI QIDQ1713670
Mohammad Nezami, Behnam Gholami
Publication date: 28 January 2019
Published in: European Journal of Mechanics. A. Solids (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/j.euromechsol.2018.11.003
Related Items (4)
The effect of magnetorheological fluid and aerodynamic damping on the flutter boundaries of MR fluid sandwich plates in supersonic airflow ⋮ Composite honeycomb sandwich columns under in-plane compression: optimal geometrical design and three-dimensional failure mechanism maps ⋮ Vibration analysis and distributed piezoelectric energy harvester design for the L-shaped beam ⋮ Size-dependent vibration analysis of an axially moving sandwich beam with MR core and axially FGM faces layers in yawed supersonic airflow
Cites Work
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- A modern course in aeroelasticity
- A finite element study of the transverse shear in honeycomb cores
- FLUTTER SUPPRESSION OF AN ELASTICALLY SUPPORTED PLATE WITH ELECTRO-RHEOLOGICAL FLUID CORE UNDER YAWED SUPERSONIC FLOWS
- Active Flutter Control of a Supersonic Honeycomb Sandwich Beam Resting on Elastic Foundation with Piezoelectric Sensor/Actuator Pair
- The forced vibration of a three-layer, damped sandwich beam with arbitrary boundary conditions
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