Flow-induced vibrations and the Landau equation

被引:6
|
作者
Schewe, Guenter [1 ]
机构
[1] Inst Aeroelast Gottingen, Deutsch Zentrum Luft & Raumfahrt DLR, D-37073 Gottingen, Germany
关键词
Flow-induced vibrations; Landau equation; Limit cycle oscillations; Transonic flutter; Bifurcations; Tacoma bridge; Aerostabil wing; CIRCULAR-CYLINDERS; TRANSONIC FLUTTER;
D O I
10.1016/j.jfluidstructs.2013.08.015
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
The initial and general transient temporal behaviours of flow induced vibrations were studied particularly with regard to the extent with which self-excited, flow-induced vibrations can be described by the Landau equation. Three different cases are studied experimentally, using bodies with generic shape. The first case represents a bluff body: resembling a simplified section of the Tacoma bridge, which has a single torsional degree of freedom. The second case is a two-dimensional airfoil in transonic flow having a heave and a torsional degree of freedom. The third case is an elastic half-wing model, also investigated in transonic flow. It is shown that in all three cases, beyond the critical point and at small initial amplitude the temporal development of the oscillations up to the limit cycle i.e. the envelope of the measured time functions, agrees with the corresponding curve, given by the solution of the Landau equation. For the Tacoma section and the airfoil the same agreement was demonstrated for initial amplitudes much larger than that of the limit cycle. In addition for both last cases the bifurcation behaviour was investigated and the Landau constants were determined. Finally an elementary physical explanation for the instability phenomenon was given. (C) 2013 Elsevier Ltd. All rights reserved.
引用
收藏
页码:256 / 270
页数:15
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