Free vibration analysis of dragonfly wings using finite element method

被引：36
|
作者：
Darvizeh, M. [1 ]
Darvizeh, A. [1 ]
Rajabi, H. [1 ]
Rezaei, A. [1 ]
机构：
[1] Guilan Univ, Dept Mech Engn, POB 3756, Rasht, Iran
来源：
INTERNATIONAL JOURNAL OF MULTIPHYSICS | 2009年 / 3卷 / 01期
关键词：
Mechanical properties; SEM; dragonfly wing; FEM; natural frequencies; damping ratio;
D O I：
10.1260/175095409787924454
中图分类号：
TH [机械、仪表工业];
学科分类号：
0802 ;
摘要：
In the present work, investigations on the microstructure and mechanical properties of the dragonfly wing are carried out and numerical modeling based on Finite Element Method (FEM) is developed to predict Flight characteristics of dragonfly wings. Vibrational behavior of wings type structures is immensely important in analysis, design and manufacturing of similar engineering structures. For this purpose natural frequencies and mode shapes are calculated. In addition, the kind of deformation in each mode shape evaluated and the ratio between numerical natural frequency and experimental natural frequency presented as damping ratio. The results obtain from present method are in good agreement with same experimental methods.
引用
收藏
页码：101 / 110
页数：10
相关论文
共 50 条
  • [1] FREE VIBRATION ANALYSIS OF A PEMFC USING THE FINITE ELEMENT METHOD
    Ahmed, Hasnet E. U.
    Zu, Jean W.
    Bazylak, Aimy
    [J]. PROCEEDINGS OF THE ASME 8TH INTERNATIONAL CONFERENCE ON FUEL CELL SCIENCE, ENGINEERING, AND TECHNOLOGY 2010, VOL 1, 2010, : 633 - 640
  • [2] Free vibration analysis of curved shells using finite element method
    Gurve, Hemant Kumar
    Satankar, Rajesh Kumar
    [J]. MATERIALS TODAY-PROCEEDINGS, 2022, 50 : 2336 - 2344
  • [3] Free Vibration Analysis of Carbon Nanotubes by Using Finite Element Method
    Dinckal, C.
    [J]. IRANIAN JOURNAL OF SCIENCE AND TECHNOLOGY-TRANSACTIONS OF MECHANICAL ENGINEERING, 2016, 40 (01) : 43 - 55
  • [4] Free vibration analysis of curved shells using finite element method
    Gurve, Hemant Kumar
    Satankar, Rajesh Kumar
    [J]. MATERIALS TODAY-PROCEEDINGS, 2022, 50 : 2336 - 2344
  • [5] Free Vibration Analysis of Carbon Nanotubes by Using Finite Element Method
    Ç. Dinçkal
    [J]. Iranian Journal of Science and Technology, Transactions of Mechanical Engineering, 2016, 40 : 43 - 55
  • [6] Comparative study on vibration characteristics of aircraft wings using finite element method
    Agrawal, Pranjal
    Dhatrak, Pankaj
    Choudhary, Paras
    [J]. MATERIALS TODAY-PROCEEDINGS, 2021, 46 : 176 - 183
  • [7] Free Vibration Analysis of Laminated Composite Plates Using Finite Element Method
    Pingulkar, Pushparaj
    Suresha, B.
    [J]. POLYMERS & POLYMER COMPOSITES, 2016, 24 (07): : 529 - 538
  • [8] Free vibration and stability analysis of piezolaminated plates using the finite element method
    Wankhade, Rajan L.
    Bajoria, Kamal M.
    [J]. SMART MATERIALS AND STRUCTURES, 2013, 22 (12)
  • [9] Free Vibration Analysis of Delaminated Composite Plates using Finite Element Method
    Ganesh, Shankar
    Kumar, Keshava S.
    Mahato, P. K.
    [J]. INTERNATIONAL CONFERENCE ON VIBRATION PROBLEMS 2015, 2016, 144 : 1067 - 1075
  • [10] Free and forced vibration analysis using the smoothed finite element method (SFEM)
    Dai, K. Y.
    Liu, G. R.
    [J]. JOURNAL OF SOUND AND VIBRATION, 2007, 301 (3-5) : 803 - 820
12345