Aerothermoelastic flutter analysis of pre-twisted thin-walled rotating blades reinforced with functionally graded carbon nanotubes

DOI10.1016/j.euromechsol.2019.01.018zbMath1472.74060OpenAlexW2912919496WikidataQ128420410 ScholiaQ128420410MaRDI QIDQ2421973

Reza Bahaadini, A. R. Saidi

Publication date: 18 June 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.2019.01.018

zbMATH Keywords

Timoshenko beamextended Galerkin methodflutter frequencysupersonic linear piston theory

Mathematics Subject Classification ID

Rods (beams, columns, shafts, arches, rings, etc.) (74K10) Vibrations in dynamical problems in solid mechanics (74H45) Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) Composite and mixture properties (74E30) Thermal effects in solid mechanics (74F05) Numerical approximation of solutions of dynamical problems in solid mechanics (74H15) Supersonic flows (76J20)

Related Items (4)

Modeling large amplitude vibration of pretwisted hybrid composite blades containing CNTRC layers and matrix cracked FRC layers ⋮ Meshless numerical approach to flutter analysis of rotating pre-twisted nanocomposite blades subjected to supersonic airflow ⋮ Size-dependent vibration analysis of an axially moving sandwich beam with MR core and axially FGM faces layers in yawed supersonic airflow ⋮ Nonlinear dynamic responses of functionally graded graphene platelet reinforced composite cantilever rotating warping plate

Cites Work

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• Free-Vibration Analysis of Rotating Beams by a Variable-Order Finite-Element Method

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