Three-dimensional nonlinear analysis and wind-tunnel experiment of flutter generated on a rectangular sheet in uniform flow

被引:15
作者
Hiroaki, K. [1 ]
Watanabe, M. [1 ]
机构
[1] Aoyama Gakuin Univ, Dept Mech Engn, Chuo Ward, 5-10-1 Fuchinobe, Sagamihara, Kanagawa 2525258, Japan
关键词
Flutter; Nonlinear analysis; Cantilevered sheet; Energy-transfer quantification; Vortex method; Limit cycle oscillation;
D O I
10.1016/j.jfluidstructs.2021.103226
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Flexible sheets are used in many industrial applications. During their manufacturing processes, the coupling of the sheet motion and airflow causes flutter, which can result in severe quality defects. To prevent these defects, a detailed understanding of the fluttering mechanisms and characteristics is essential. In this study, wind-tunnel experiments and three-dimensional nonlinear flutter analysis are carried out on a cantilevered rectangular sheet in uniform flow. The post-critical behavior of the sheets (flutter amplitudes, frequencies and modes) is examined in detail. The influence of structural damping and fluid friction on the post-critical behavior is carefully investigated for various mass ratios through the nonlinear analysis. Finally, the work done by the fluid force acting on the sheet surface is examined through nonlinear analysis to understand the sustaining mechanism of limit cycle oscillation (LCO). It is found that the competition between the positive and negative work done by the fluid force contributes considerably to the sustaining mechanism of the LCO. (C) 2021 Elsevier Ltd. All rights reserved.
引用
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页数:24
相关论文
共 31 条
[1]   Bifurcation and chaos of a flag in an inviscid flow [J].
Chen, Ming ;
Jia, Lai-Bing ;
Wu, Yan-Feng ;
Yin, Xie-Zhen ;
Ma, Yan-Bao .
JOURNAL OF FLUIDS AND STRUCTURES, 2014, 45 :124-137
[2]   Skin friction on a flapping plate in uniform flow [J].
Ehrenstein, Uwe ;
Marquillie, Matthieu ;
Eloy, Christophe .
PHILOSOPHICAL TRANSACTIONS OF THE ROYAL SOCIETY A-MATHEMATICAL PHYSICAL AND ENGINEERING SCIENCES, 2014, 372 (2020)
[3]   Flutter of a rectangular plate [J].
Eloy, C. ;
Souilliez, C. ;
Schouveiler, L. .
JOURNAL OF FLUIDS AND STRUCTURES, 2007, 23 (06) :904-919
[4]   Aeroelastic instability of cantilevered flexible plates in uniform flow [J].
Eloy, Christophe ;
Lagrange, Romain ;
Souilliez, Claire ;
Schouveiler, Lionel .
JOURNAL OF FLUID MECHANICS, 2008, 611 :97-106
[5]   The origin of hysteresis in the flag instability [J].
Eloy, Christophe ;
Kofman, Nicolas ;
Schouveiler, Lionel .
JOURNAL OF FLUID MECHANICS, 2012, 691 :583-593
[6]   Theory and experiment for flutter of a rectangular plate with a fixed leading edge in three-dimensional axial flow [J].
Gibbs, S. Chad ;
Wang, Ivan ;
Dowell, Earl .
JOURNAL OF FLUIDS AND STRUCTURES, 2012, 34 :68-83
[7]   Stability of rectangular plates with free side-edges in two-dimensional inviscid channel flow [J].
Guo, CQ ;
Paidoussis, MP .
JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME, 2000, 67 (01) :171-176
[8]  
Hiroaki K, 2015, PROCEEDINGS OF THE ASME PRESSURE VESSELS AND PIPING CONFERENCE - 2015, VOL 4
[9]   A RECURRENCE MATRIX SOLUTION FOR THE DYNAMIC RESPONSE OF ELASTIC AIRCRAFT [J].
HOUBOLT, JC .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1950, 17 (09) :540-&
[10]   Interaction between a cantilevered-free flexible plate and ideal flow [J].
Howell, R. M. ;
Lucey, A. D. ;
Carpenter, P. W. ;
Pitman, M. W. .
JOURNAL OF FLUIDS AND STRUCTURES, 2009, 25 (03) :544-566