EXPERIMENTAL AEROELASTIC BEHAVIOR OF UNSWEPT AND FORWARD-SWEPT CANTILEVER GRAPHITE EPOXY WINGS

被引:17
作者
LANDSBERGER, BJ
DUGUNDJI, J
机构
来源
JOURNAL OF AIRCRAFT | 1985年 / 22卷 / 08期
关键词
D O I
10.2514/3.45186
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:679 / 686
页数:8
相关论文
共 21 条
[1]  
Ashton JE, 1970, THEORY LAMINATED PLA
[2]  
Bisplinghoff R.L., 1996, AEROELASTICITY
[3]   SWEPT COMPOSITE WING AEROELASTIC DIVERGENCE EXPERIMENTS [J].
BLAIR, M ;
WEISSHAAR, TA .
JOURNAL OF AIRCRAFT, 1982, 19 (11) :1019-1024
[4]  
DEYOUNG J, 1948, NACA921 REPT
[5]  
DUGUNDJI J, 1974, AFOSR TR741734 AIR F
[6]  
DUGUNDJI J, ASLTR1596 MIT AER ST
[7]  
DUGUNDJI J, ASRL TR1801 MIT AER
[8]  
DUGUNDJI J, 1975, NASA CR144924
[9]  
HERTZ TJ, 1982, ASTRONAUT AERONAUT, V20, P40
[10]   AEROELASTIC FLUTTER AND DIVERGENCE OF STIFFNESS COUPLED, GRAPHITE EPOXY CANTILEVERED PLATES [J].
HOLLOWELL, SJ ;
DUGUNDJI, J .
JOURNAL OF AIRCRAFT, 1984, 21 (01) :69-76