Free vibration analysis of laminated composite and sandwich shells using wavelet finite element method

被引:6
作者
Garg, Aman [1 ,2 ]
Sabherwal, Pooja [2 ]
Shukla, Neeraj Kumar [3 ,4 ]
Li, Li [1 ]
Raja, M. Ramkumar [3 ,4 ]
Sharma, Anshu [5 ]
Raman, Roshan [2 ]
Chalak, H. D. [6 ]
机构
[1] Huazhong Univ Sci & Technol, Sch Mech Sci & Engn, State Key Lab Intelligent Mfg Equipment & Technol, Wuhan 430074, Peoples R China
[2] NorthCap Univ, Dept Multidisciplinary Engn, Gurugram, Haryana, India
[3] King Khalid Univ, Coll Engn, Dept Elect Engn, Abha, Saudi Arabia
[4] King Khalid Univ, Ctr Engn & Technol Innovat, Abha, Saudi Arabia
[5] Kangwon Natl Univ, Dept Chem Engn, Chuncheon Si, Gangwon Do, South Korea
[6] Natl Inst Technol Kurukshetra, Dept Civil Engn, Kurukshetra, Haryana, India
关键词
Wavelet finite element method; higher-order zigzag theory; Haar wavelet; BSWI wavelet; doubly-curved shells and panels; frequency; REFINED THEORY; PLATES; BEAMS; FORMULATION;
D O I
10.1080/15376494.2024.2380090
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The present work carries out free vibration analysis of laminated composite shells and panels using wavelet finite element method (WFEM). Two different wavelets, namely, Haar and B-spline wavelet on the interval (BSWI) are employed. The analysis is carried out using higher-order zigzag theory (HOZT), and the WFEM is set up according to Hamilton's principle. The two-dimensional scaling functions are employed to substitute the interpolation functions as used in the FEM. Owing to the capability of the WFEM to work efficiently with lesser degrees of freedom compared to the traditional FEM, the proposed methodology is validated with the results available.
引用
收藏
页码:2439 / 2447
页数:9
相关论文
共 66 条
[1]   Rotordynamic analyses of stiffened cylindrical structures using high-fidelity shell models [J].
Azzara, R. ;
Filippi, M. ;
Carrera, E. .
MECHANICS OF ADVANCED MATERIALS AND STRUCTURES, 2024, 31 (29) :11677-11686
[2]  
Biswal M, 2016, STEEL COMPOS STRUCT, V22, P1445, DOI [10.12989/scs.2016.22.6.1463, 10.12989/scs.2016.22.6.1445]
[3]   Vibration of metallic and composite shells in geometrical nonlinear equilibrium states [J].
Carrera, E. ;
Pagani, A. ;
Azzara, R. ;
Augello, R. .
THIN-WALLED STRUCTURES, 2020, 157 (157)
[4]   Finite elements based on Jacobi shape functions for the free vibration analysis of beams, plates, and shells [J].
Carrera, Erasmo ;
Scano, Daniele .
MECHANICS OF ADVANCED MATERIALS AND STRUCTURES, 2024, 31 (01) :4-12
[5]   Carrera Unified Formulation for Free-Vibration Analysis of Aircraft Structures [J].
Carrera, Erasmo ;
Zappino, Enrico .
AIAA JOURNAL, 2016, 54 (01) :280-292
[6]   Bending, free vibrations and buckling of laminated composite and sandwich plates using a layerwise displacement model [J].
Cetkovic, M. ;
Vuksanovic, Dj. .
COMPOSITE STRUCTURES, 2009, 88 (02) :219-227
[7]   Stability Analysis of Laminated Soft Core Sandwich Plates Using Higher Order Zig-Zag Plate Theory [J].
Chalak, H. D. ;
Chakrabarti, Anupam ;
Sheikh, Abdul Hamid ;
Iqbal, Mohd. Ashraf .
MECHANICS OF ADVANCED MATERIALS AND STRUCTURES, 2015, 22 (11) :897-907
[8]   Free Vibration Analysis of Laminated Soft Core Sandwich Plates [J].
Chalak, H. D. ;
Chakrabarti, Anupam ;
Iqbal, Mohd. Ashraf ;
Sheikh, Abdul Hamid .
JOURNAL OF VIBRATION AND ACOUSTICS-TRANSACTIONS OF THE ASME, 2013, 135 (01)
[9]   Vibration of laminated sandwich beams having soft core [J].
Chalak, Hanuman Devidas ;
Chakrabarti, Anupam ;
Iqbal, Mohamad Asharaf ;
Sheikh, Abdul Hamid .
JOURNAL OF VIBRATION AND CONTROL, 2012, 18 (10) :1422-1435
[10]   Free-vibration analysis of laminated shells via refined MITC9 elements [J].
Cinefra, M. .
MECHANICS OF ADVANCED MATERIALS AND STRUCTURES, 2016, 23 (09) :937-947