Vibration characteristics of rotating pretwisted composite tapered blade with graphene coating layers

被引:106
作者
Zhang, W. [1 ]
Niu, Y. [1 ]
Behdinan, K. [2 ]
机构
[1] Beijing Univ Technol, Coll Mech Engn, Beijing Key Lab Nonlinear Vibrat & Strength Mech, Beijing 100124, Peoples R China
[2] Univ Toronto, Dept Mech & Ind Engn, Adv Res Lab Multifunct Light Weight Struct, 5 Kings Coll Rd, Toronto, ON M5S 3G8, Canada
基金
中国国家自然科学基金;
关键词
Pretwisted tapered cylindrical panel; Graphene coating layer; Rotating speed; Frequency veering; NONLINEAR VIBRATION; ELASTIC FOUNDATIONS; FORCED VIBRATIONS; DYNAMIC-ANALYSIS; MODAL-ANALYSIS; PLATES; MODEL; BEAMS;
D O I
10.1016/j.ast.2019.105644
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A new dynamic model of the rotating tapered cantilever cylindrical panel with the graphene coating layers is developed to investigate the vibration characteristics of the rotating pretwisted tapered blade. It is assumed that the graphene platelets (GPLs) are randomly oriented and uniformly dispersed in the top layer and the bottom layer of the rotating pretwisted composite tapered blade. The modified Halpin-Tsai model is used to estimate the effective Young's modulus. The rule of the mixture is used to calculate the effective Poisson's ratio and mass density. Based on the Green strain tensor, an accurate strain-displacement relationship is acquired. The effects of the centrifugal force and Coriolis force are considered in the formulation. The Chebyshev-Ritz method is utilized to obtain the natural frequencies and mode shapes of the rotating pretwisted composite tapered blade with the graphene coating layers. The accuracy of the proposed model is validated through several comparison studies with the results of the present literatures and ANSYS. The free vibration characteristics are analyzed by considering different material and geometry parameters of the rotating pretwisted composite tapered cantilever cylindrical panel with the graphene coating layers, such as the graphene platelet (GPL) geometry, GPL weight fraction, taper ratio, length-to-radius ratio, pretwist angle, presetting angle and rotating speed. The frequency veering and the mode shape shift phenomena are found in the rotating pretwisted tapered cantilever cylindrical panel with the graphene coating layers. (C) 2019 Elsevier Masson SAS. All rights reserved.
引用
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页数:20
相关论文
共 48 条
[1]   Free vibration analysis of a pre-twisted sandwich blade with thermal barrier coatings layers [J].
Cao DongXing ;
Liu BingYi ;
Yao MingHui ;
Zhang Wei .
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2017, 60 (11) :1747-1761
[2]   Vibration characteristics of a rotating pre-twisted composite laminated blade [J].
Chen, Jie ;
Li, Qiu-Sheng .
COMPOSITE STRUCTURES, 2019, 208 :78-90
[3]   Vibration and damping analysis of the bladed disk with damping hard coating on blades [J].
Chen, Yugang ;
Zhai, Jingyu ;
Han, Qingkai .
AEROSPACE SCIENCE AND TECHNOLOGY, 2016, 58 :248-257
[4]   Comparison of natural frequencies of laminates by 3-D theory, part II: Curved panels [J].
Chern, YC ;
Chao, CC .
JOURNAL OF SOUND AND VIBRATION, 2000, 230 (05) :1009-1030
[5]   Nano-indentation studies on polymer matrix composites reinforced by few-layer graphene [J].
Das, Barun ;
Prasad, K. Eswar ;
Ramamurty, U. ;
Rao, C. N. R. .
NANOTECHNOLOGY, 2009, 20 (12)
[6]   Vibration analysis of rotating functionally graded tapered beams with hollow circular cross-section [J].
Dong, Shipeng ;
Li, Liang ;
Zhang, Dingguo .
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 95
[7]   Buckling of spinning functionally graded graphene reinforced porous nanocomposite cylindrical shells: analytical study [J].
Dong, Y. H. ;
He, L. W. ;
Wang, L. ;
Li, Y. H. ;
Yang, J. .
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 82-83 :466-478
[8]  
Ghosh S, 2010, NAT MATER, V9, P555, DOI [10.1038/nmat2753, 10.1038/NMAT2753]
[9]   Free vibration of rotating cantilever pre-twisted panel with initial exponential function type geometric imperfection [J].
Gu, X. J. ;
Hao, Y. X. ;
Zhang, W. ;
Liu, L. T. ;
Chen, J. .
APPLIED MATHEMATICAL MODELLING, 2019, 68 :327-352
[10]   Internal Resonance Responses of Rectangular Cross-Ply Composite Plates with Graphene Skins [J].
Guo, Xiangying ;
Jiang, Pan ;
Yan, Wenhan ;
Lai, Siu-Kai ;
Zhang, Wei .
INTERNATIONAL JOURNAL OF STRUCTURAL STABILITY AND DYNAMICS, 2019, 19 (06)