Influence of nonlinear viscoelastic material characterization on performance of constrained layer damping treatment

被引:11
作者
Gandhi, F [1 ]
机构
[1] Penn State Univ, Dept Aerosp Engn, University Pk, PA 16802 USA
关键词
D O I
10.2514/2.1397
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The influence of nonlinear viscoelastic material behavior on the performance of a passive constrained layer damping treatment is examined. For numerical simulations, a finite element model of a beam, simply supported at both ends, and with symmetric constrained layer damping treatments on the top and bottom surfaces, is considered. Results indicate that, if the viscoelastic material is relatively compliant, the damping provided by the treatment will decrease for increasing excitation levels, due primarily to the reduction in the viscoelastic material shear loss modulus, However, if the viscoelastic material is relatively stiff, the damping provided by the treatment will increase for increasing excitation levels, due primarily to increased shear in the viscoelastic laver associated with the decrease in its shear storage modulus, The benefits obtained by segmentation of the constrained layer damping treatment were seen to reduce substantially when the nonlinear behavior of the viscoelastic material was considered.
引用
收藏
页码:924 / 931
页数:8
相关论文
共 16 条
[1]   Use of active constrained-layer damping for controlling resonant vibration [J].
Azvine, B. ;
Tomlinson, G.R. ;
Wynne, R.J. .
Smart Materials and Structures, 1995, 4 (01) :1-6
[2]   OPTIMUM DESIGN AND CONTROL OF ACTIVE CONSTRAINED LAYER DAMPING [J].
BAZ, A ;
RO, J .
JOURNAL OF MECHANICAL DESIGN, 1995, 117 :135-144
[3]  
BAZ A, P DAMP 93 IBB SAN FR, P1
[4]  
Felker F.F., 1987, J AM HELICOPTER SOC, V32,, P45, DOI DOI 10.4050/JAHS.32.45
[5]   Analysis of bearingless main rotor aeroelasticity using an improved time domain nonlinear elastomeric damper model [J].
Gandhi, F ;
Chopra, I .
JOURNAL OF THE AMERICAN HELICOPTER SOCIETY, 1996, 41 (03) :267-277
[6]   ANALYTICAL MODEL FOR A NONLINEAR ELASTOMERIC LAG DAMPER AND ITS EFFECT ON AEROMECHANICAL STABILITY IN HOVER [J].
GANDHI, F ;
CHOPRA, I .
JOURNAL OF THE AMERICAN HELICOPTER SOCIETY, 1994, 39 (04) :59-69
[7]   A time-domain non-linear viscoelastic damper model [J].
Gandhi, F ;
Chopra, I .
SMART MATERIALS & STRUCTURES, 1996, 5 (05) :517-528
[8]  
HAUSMANN G, 1992, P 18 EUR ROT FOR AV
[9]  
HAUSMANN G, 1986, P 12 EUR ROT FOR
[10]   Some design considerations for active and passive constrained layer damping treatments [J].
Huang, SC ;
Inman, DJ ;
Austin, EM .
SMART MATERIALS & STRUCTURES, 1996, 5 (03) :301-313