DYNAMIC TRANSFORMATION METHOD FOR MODAL SYNTHESIS

被引:61
作者
KUHAR, EJ [1 ]
STAHLE, CV [1 ]
机构
[1] GE,VALLEY FORGE,PA 19481
关键词
D O I
10.2514/3.49318
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
引用
收藏
页码:672 / 678
页数:7
相关论文
共 15 条
[1]  
BAJAN RL, 1968, AAS6881 PAP
[2]  
BAJAN RL, 1968, 39 P SHOCK VIBR S MO
[3]   VIBRATION ANALYSIS OF STRUCTURES BY COMPONENT MODE SUBSTITUTION [J].
BENFIELD, WA ;
HRUDA, RF .
AIAA JOURNAL, 1971, 9 (07) :1255-&
[4]  
BENFIELD WA, 1972, AUG P S SUBSTR TEST
[5]  
COKONIS TJ, 1972, 42 NAV RES LAB SHO 4
[6]   COUPLING OF SUBSTRUCTURES FOR DYNAMIC ANALYSES [J].
CRAIG, RR ;
BAMPTON, MCC .
AIAA JOURNAL, 1968, 6 (07) :1313-&
[7]   VIBRATION ANALYSIS BY DYNAMIC PARTITIONING [J].
GOLDMAN, RL .
AIAA JOURNAL, 1969, 7 (06) :1152-&
[8]   RUDUCTION OF STIFFNESS AND MASS MATRICES [J].
GUYAN, RJ .
AIAA JOURNAL, 1965, 3 (02) :380-&
[9]  
HART GC, 1971, SEP P NAT AER SPAC E
[10]  
HOU SN, 1969, 40 NAV RES LAB SHOCK