Frequency response of beams with passively constrained damping layers and piezo-actuators
被引:11
作者:
Wang, G
论文数: 0引用数: 0
h-index: 0
机构:
Univ Maryland, Dept Aerosp Engn, Alfred Gessow Rotorcraft Ctr, Smart Struct Lab, College Pk, MD 20742 USAUniv Maryland, Dept Aerosp Engn, Alfred Gessow Rotorcraft Ctr, Smart Struct Lab, College Pk, MD 20742 USA
Wang, G
[1
]
Wereley, NM
论文数: 0引用数: 0
h-index: 0
机构:
Univ Maryland, Dept Aerosp Engn, Alfred Gessow Rotorcraft Ctr, Smart Struct Lab, College Pk, MD 20742 USAUniv Maryland, Dept Aerosp Engn, Alfred Gessow Rotorcraft Ctr, Smart Struct Lab, College Pk, MD 20742 USA
Wereley, NM
[1
]
机构:
[1] Univ Maryland, Dept Aerosp Engn, Alfred Gessow Rotorcraft Ctr, Smart Struct Lab, College Pk, MD 20742 USA
来源:
PASSIVE DAMPING AND ISOLATION - SMART STRUCTURES AND MATERIALS 1998
|
1998年
/
3327卷
关键词:
D O I:
10.1117/12.310712
中图分类号:
O42 [声学];
学科分类号:
070206 ;
082403 ;
摘要:
We present and review methods of frequency response analysis for cantilevered sandwich beams consisting of aluminum face plates and passively constrained damping layers at the mid-plane. These analysis methods include: (1) progressive wave method, (2) assumed modes method, and (3) finite element method. The progressive wave method accounts for the frequency dependent complex modulus in analyzing the frequency response function. In the assumed made and FEM analyses, the frequency dependent complex modulus is assumed to be a constant over the frequency range of interest (i.e. the first three modes). By selecting the value of complex modulus to nominally correspond to the second modal frequency, the error in predicted natural frequency can be minimized. However, this comes at the cost of increased error in the damping ratio predictions, which are minimized by selecting the value of complex modulus corresponding to the first mode.