Aerothermoelastic analysis of GPL-reinforced composite lattice sandwich beams based on a refined equivalent model
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Publication:6044001
DOI10.1016/J.ENGANABOUND.2023.02.001zbMath1521.74128OpenAlexW4319763540MaRDI QIDQ6044001
Chunxiao Wang, Yaze Liu, Yuewu Wang
Publication date: 25 May 2023
Published in: Engineering Analysis with Boundary Elements (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/j.enganabound.2023.02.001
supersonic airflowflutter propertiesgraphene platelets (GPLs) reinforced composite materiallattice sandwich beamnonuniform thermal environments
Cites Work
- Meshless numerical approach to flutter analysis of rotating pre-twisted nanocomposite blades subjected to supersonic airflow
- Low-velocity impact response of sandwich plates with GRC face sheets and FG auxetic 3D lattice cores
- Mechanical and energy absorption properties of the composite XX-type lattice sandwich structure
- Nonlinear primary resonances of lattice sandwich beams with pyramidal truss core and viscoelastic surfaces
- An energy approach to the solution of partial differential equations in computational mechanics via machine learning: concepts, implementation and applications
- Aeroelastic analysis and active flutter control of nonlinear lattice sandwich beams
- Collapse of truss core sandwich beams in 3-point bending
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