MULTIPLE ACCEPTABLE SOLUTIONS IN STRUCTURAL MODEL IMPROVEMENT

被引:24
作者
BERMAN, A
机构
[1] Bloomfield, CT, 06002
关键词
D O I
10.2514/3.12657
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper examines the question as to whether it is possible to obtain the correct discrete linear analytical model of an actual structure by the use of analysis and test data. It is shown that no such correct model exists. an illustration of an application is shown where multiple acceptable and very different analytical models are all representative of the structure. The implications regarding methods of improving analytical models and detecting damage are discussed.
引用
收藏
页码:924 / 927
页数:4
相关论文
共 9 条
[1]   OPTIMAL WEIGHTED ORTHOGONALIZATION OF MEASURED MODES [J].
BARUCH, M ;
BARITZHACK, IY .
AIAA JOURNAL, 1978, 16 (04) :346-351
[2]   IMPROVEMENT OF A LARGE ANALYTICAL MODEL USING TEST DATA [J].
BERMAN, A ;
NAGY, EJ .
AIAA JOURNAL, 1983, 21 (08) :1168-1173
[3]  
BERMAN A, 1987, VERTICA, V11, P309
[4]  
BERMAN A, 1973, SHOCK VIBRATION B, V43, P13
[5]  
BERMAN A, 1984, 2ND INT C REC ADV ST
[6]  
BERMAN A, 1984, AIAA840929 PAP
[7]   ANALYTICAL MODEL IMPROVEMENT USING MODAL TEST-RESULTS [J].
CHEN, JC ;
GARBA, JA .
AIAA JOURNAL, 1980, 18 (06) :684-690
[8]   RUDUCTION OF STIFFNESS AND MASS MATRICES [J].
GUYAN, RJ .
AIAA JOURNAL, 1965, 3 (02) :380-&
[9]   STIFFNESS AND DEFLECTION ANALYSIS OF COMPLEX STRUCTURES [J].
TURNER, MJ ;
CLOUGH, RW ;
MARTIN, HC ;
TOPP, LJ .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1956, 23 (09) :805-&