Estimation of reciprocal residual flexibility from experimental modal data

被引:43
作者
Doebling, SW
Peterson, LD
Alvin, KF
机构
[1] UNIV COLORADO,DEPT AEROSP ENGN SCI,BOULDER,CO 80309
[2] SANDIA NATL LABS,STRUCT DYNAM & VIBRAT CONTROL DEPT,ALBUQUERQUE,NM 87185
关键词
D O I
10.2514/3.13289
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A technique is presented for estimating the residual flexibility between nonexcited structural degrees of freedom from experimental structural vibration data. Using this method, one can include the residual flexibility estimated from modal measurements in the computation of measured flexibility for experiments with incomplete reciprocity, i.e., when the response and excitation measurement sensors are not fully collocated. The method can also be used to estimate the unknown entries in the residual flexibility matrix for experimental component mode synthesis when excitations are not provided at all interface degrees of freedom. A general solution is presented that contains an unknown positive semidefinite contribution. The general solution satisfies modal orthogonality in the limit that all of the structural degrees of freedom are instrumented and when the positive semidefinite contribution lies in a nullspace defined by the stiffness matrix and the modal flexibility. With a limited number of measurements, modal orthogonality is shown to be satisfied to the extent that the measured modes are preserved by static condensation. A rank-deficient solution is presented that allows the residual to be used in the computation of the flexibility matrix without further modeling assumptions. Numerical and experimental results that demonstrate the application of the method to both flexibility matrix convergence and experimental component mode synthesis are presented.
引用
收藏
页码:1678 / 1685
页数:8
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