Meshless numerical approach to flutter analysis of rotating pre-twisted nanocomposite blades subjected to supersonic airflow
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Publication:1980179
DOI10.1016/j.enganabound.2021.07.008OpenAlexW3186252591MaRDI QIDQ1980179
Krzysztof Kamil Żur, Xu Ouyang, Hulun Guo, Xintao Wu
Publication date: 3 September 2021
Published in: Engineering Analysis with Boundary Elements (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/j.enganabound.2021.07.008
flutterelement-free IMLS-Ritz methodgraphene nanoplateletsnanocomposite platesrotating pre-twisted blades
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Cites Work
- Nonlinear dynamic responses of rotating pretwisted cylindrical shells
- Meshfree simulation of temperature effects on the mechanical behaviors of microtubules
- Active aeroelastic flutter suppression of a supersonic plate with piezoelectric material
- Vibration of turbomachinery rotating blades made-up of functionally graded materials and operating in a high temperature field
- Nonlinear vibration analysis of composite blade with variable rotating speed using Chebyshev polynomials
- Modeling and dynamic study of rotating blades with adjustable stagger angle
- Free vibration of rotating pretwisted functionally graded composite cylindrical panel reinforced with graphene platelets
- Aerothermoelastic flutter analysis of pre-twisted thin-walled rotating blades reinforced with functionally graded carbon nanotubes
- Free vibration analysis of Timoshenko beams by DSC method
- Flutter analysis of stiffened laminated composite plates and shells in supersonic flow
- Finite element flutter analysis of composite skew panels
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