Modal Analysis of Monolithic and Jointed Type Cantilever Beams with Non-Uniform Section

被引:6
作者
Purohit, Bimal [1 ]
Jain, Prakash Chand [2 ]
Pandey, Ashok Kumar [1 ]
机构
[1] Indian Inst Technol Hyerabad, Mech & Aerosp Engn, Vehicle Dynam Lab, Kandi, India
[2] Def Res & Dev Lab, Flight Struct Div, Hyderabad, Andhra Pradesh, India
关键词
Non-uniform beam; Bolted structures; Model analysis; Closed form solution; BOLTED JOINTS; VIBRATION; DYNAMICS; IDENTIFICATION; MISSILES; SYSTEMS;
D O I
10.1007/s11340-016-0149-y
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Modal analysis of non-uniform bolted structures are of significance in modeling many complex mechanical structures. There are vast literatures available related with the analytical as well as numerical modeling of bolted joint. However, most of the analytical model discuss about the modeling of first mode of uniform structures with single bolted joint. In this paper, we present the modeling of single as well as bolted non-uniform beams using approximate mode shapes. To develop the model, we first carry out experiments to measures the modal frequencies and shapes of the test structures. Subsequently, we also do numerical modeling of non-uniform beams in ANSYS to verify the validity of the Euler-Bernoulli beam theory in developing the analytical models. Finally, using the Euler-Bernoulli beam theory, we obtain the analytical values of frequencies using the approximate the mode shapes. The analytical results are found to be closer to the experimental results with a maximum percentage error of about 15 %. The model presented in the paper can be extended to the mechanical structures with many non-uniform sections with or without bolted joints.
引用
收藏
页码:1083 / 1094
页数:12
相关论文
共 27 条
[11]   An adaptive harmonic balance method for predicting the nonlinear dynamic responses of mechanical systems-Application to bolted structures [J].
Jaumouille, V. ;
Sinou, J. -J. ;
Petitjean, B. .
JOURNAL OF SOUND AND VIBRATION, 2010, 329 (19) :4048-4067
[12]   Free vibration of a cantilevered beam with multiple steps: Comparison of several theoretical methods with experiment [J].
Jaworski, J. W. ;
Dowell, E. H. .
JOURNAL OF SOUND AND VIBRATION, 2008, 312 (4-5) :713-725
[13]   Identification of bolted joints through laser vibrometry [J].
Ma, X ;
Bergman, L ;
Vakakis, A .
JOURNAL OF SOUND AND VIBRATION, 2001, 246 (03) :441-460
[14]   Simplified models of bolted joints under harmonic loading [J].
Oldfield, M ;
Ouyang, H ;
Mottershead, JE .
COMPUTERS & STRUCTURES, 2005, 84 (1-2) :25-33
[15]   Experimental and theoretical studies of a bolted joint excited by a torsional dynamic load [J].
Ouyang, H. ;
Oldfield, M. J. ;
Mottershead, J. E. .
INTERNATIONAL JOURNAL OF MECHANICAL SCIENCES, 2006, 48 (12) :1447-1455
[16]   Non-linear structural dynamics characterization using a scanning laser vibrometer [J].
Pai, PF ;
Lee, SY .
JOURNAL OF SOUND AND VIBRATION, 2003, 264 (03) :657-687
[17]   AEROELASTIC STABILITY OF SLENDER, SPINNING MISSILES [J].
PLATUS, DH .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1992, 15 (01) :144-151
[18]   Investigation of thrust effect on the vibrational characteristics of flexible guided missiles [J].
Pourtakdoust, SH ;
Assadian, N .
JOURNAL OF SOUND AND VIBRATION, 2004, 272 (1-2) :287-299
[19]   Dynamic instability characteristics of a free-free missile structure under a controlled follower force [J].
Pradhan, Sumeet ;
Datta, P. K. .
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2006, 78 (06) :509-514
[20]   Modal analysis of jointed structures [J].
Quinn, D. Dane .
JOURNAL OF SOUND AND VIBRATION, 2012, 331 (01) :81-93