LATERAL BENDING-TORSION VIBRATIONS OF A THIN BEAM UNDER PARAMETRIC EXCITATION

被引:50
作者
DUGUNDJI, J [1 ]
MUKHOPADHYAY, V [1 ]
机构
[1] MIT, DEPT AERONAUT & ASTRONAUT, CAMBRIDGE, MA 02139 USA
来源
JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME | 1973年 / 40卷 / 03期
关键词
Combination resonance - Forcing frequencies - Governing equations - Harmonic excitation - Parametric excitations - Primary instability - Torsion vibration - Vibration testing;
D O I
10.1115/1.3423075
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
A thin platelike cantilever beam, well below static lateral buckling under gravity, is subjected to vertical harmonic excitation of its base. The governing equations indicate combination resonance possible, where the primary instability regions occur near forcing frequencies ωF = Ωi + Ωj, and each mode oscillates at its own natural frequency, Ω i. Experimental results are given for an actual beam showing this behavior. Since the beam had nonlinear damping, the instability regions settled down to steady nonlinear limit cycles whose frequencies and also amplitudes were well predicted by theory. This example of simultaneous excitation of two modes, each oscillating steadily at its own natural frequency, may be of considerable interest in vibration testing of actual structures. © 1973 by ASME.
引用
收藏
页码:693 / 698
页数:6
相关论文
共 12 条
  • [1] Bolotin V.V., 1964, DYNAMIC STABILITY EL
  • [2] Bolotin VV, 1963, NONCONSERVATIVE PROB
  • [3] THEROETICAL CONSIDERATIONS OF PANEL FLUTTER AT HIGH SUPERSONIC MACH NUMBERS
    DUGUNDJI, J
    [J]. AIAA JOURNAL, 1966, 4 (07) : 1257 - &
  • [4] Dugundji J., 1970, Revue Roumaine des Sciences Techniques, Serie de Mecanique Appliquee, V15, P741
  • [5] DUGUNDJI J, 1969, AIAA J, V7, P1663, DOI 10.2514/3.55515
  • [6] DUGUNDJI J, 1972, TR1594 MIT AER STRUC
  • [7] EVANSTON HA, 1966, T ASME E, V88, P141
  • [8] HERRMANN G, DYNAMIC STABILITY ST
  • [9] HSU CS, 1963, T ASME E, V85, P367
  • [10] MUKHOPADHAYA V, 1970, THESIS MIT