DYNAMIC RESPONSE OF A CYLINDRICAL SHELL - 2 NUMERICAL METHODS

被引:25
作者
JOHNSON, DE
GREIF, R
机构
关键词
D O I
10.2514/3.3462
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:486 / &
相关论文
共 9 条
[1]  
BALMER HA, 1964, DFLTDR64108 TECH DOC
[2]  
Bisplinghoff R. L., 1957, AEROELASTICITY
[3]   NUMERICAL ANALYSIS OF UNSYMMETRICAL BENDING OF SHELLS OF REVOLUTION [J].
BUDIANSKY, B ;
RADKOWSKI, PP .
AIAA JOURNAL, 1963, 1 (08) :1833-1842
[4]   A RECURRENCE MATRIX SOLUTION FOR THE DYNAMIC RESPONSE OF ELASTIC AIRCRAFT [J].
HOUBOLT, JC .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1950, 17 (09) :540-&
[5]  
LEVY S, 1951, 1 P US NAT C APPL ME, V1
[6]   NUMERICAL ANALYSIS OF EQUATIONS OF THIN SHELLS OF REVOLUTION [J].
RADKOWSKI, PP ;
DAVIS, RM ;
BOLDUC, MR .
ARS JOURNAL, 1962, 32 (01) :36-41
[7]  
SANDERS JL, 1959, 24 NASA REPT
[8]   LARGE DYNAMIC DEFORMATIONS OF BEAMS, RINGS, PLATES, AND SHELLS [J].
WITMER, EA ;
BALMER, HA ;
LEECH, JW ;
PIAN, THH .
AIAA JOURNAL, 1963, 1 (08) :1848-1857
[9]  
YAO JC, 1965, 65111 AIAA PREPR