Nonlinear time domain and stability analysis of beams under partially distributed follower force

被引:6
|
作者
Izadpanahi, Ehsan [1 ]
Rastkar, Siavash [1 ]
Zisis, Ioannis [2 ]
Fazelzadeh, S. Ahmad [3 ]
Mardanpour, Pezhman [1 ]
机构
[1] Florida Int Univ, Dept Mech & Mat Engn, 10555 W Flagler St, Miami, FL 33174 USA
[2] Florida Int Univ, Dept Civil & Environm Engn, 10555 W Flagler St, Miami, FL 33174 USA
[3] Shiraz Univ, Sch Mech Engn, Shiraz 7196316548, Iran
关键词
Partially distributed follower force; Nonlinear dynamic analysis; Geometrically exact beam formulation; DYNAMIC INSTABILITY CHARACTERISTICS; CANTILEVER BEAM; GEOMETRICALLY EXACT; LARGE DEFLECTIONS; FLIGHT DYNAMICS; CONVEYING FLUID; CURVED PANELS; FLUTTER; ENGINE; EQUATIONS;
D O I
10.1016/j.apm.2019.04.031
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
This paper aims to investigate linear and nonlinear behavior of beams subjected to externally applied partially distributed follower forces. In this investigation, the nonlinear composite beam theory of Hodges is used. The system of nonlinear equations is linearized about the equilibrium, or rest structure state, and the linear system is solved numerically. The effects of follower force position on the behavior of eigenvalues at pre- and post-instability are reported. Additionally, the contours of critical follower force are obtained by changing the position of follower force in span-wise and chord-wise directions. The effects of different parameters such as the length, and position of follower force and the ratios of stiffnesses on the critical follower force as well as the nonlinear limit cycle oscillation (LCO) are reported. The obtained results indicate that the length and the position of the partially distributed follower forces considerably affect the stability of the beam. (C) 2019 Elsevier Inc. All rights reserved.
引用
收藏
页码:303 / 326
页数:24
相关论文
共 50 条