COUPLED BENDING-TORSION FLUTTER IN CASCADES

被引:47
作者
BENDIKSEN, O [1 ]
FRIEDMANN, P [1 ]
机构
[1] PACIFIC AIRMOT CORP,BURBANK,CA
关键词
D O I
10.2514/3.50748
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
28
引用
收藏
页码:194 / 201
页数:8
相关论文
共 28 条
[1]  
BENDIKSEN O, 1979, AIAA790793 PAP
[2]  
Bisplinghoff R.L., 1955, AEROELASTICITY, P532
[3]  
Bolotin VV, 1963, NONCONSERVATIVE PROB
[4]  
Carta F.O., 1967, J ENG POWER, P419
[5]   THE EQUATION OF ENERGY BALANCE FOR FLUTTERING SYSTEMS WITH SOME APPLICATIONS IN THE SUPERSONIC REGIME [J].
CRISP, JDC .
JOURNAL OF THE AEROSPACE SCIENCES, 1959, 26 (11) :703-&
[6]  
DYE R, 1969, J ENG POWER JUL, P182
[7]   INFLUENCE OF MISTUNING ON ROTOR-BLADE VIBRATIONS [J].
ELBAYOUMY, LE ;
SRINIVASAN, AV .
AIAA JOURNAL, 1975, 13 (04) :460-464
[8]   RECENT DEVELOPMENTS IN ROTARY-WING AEROELASTICITY [J].
FRIEDMANN, PP .
JOURNAL OF AIRCRAFT, 1977, 14 (11) :1027-1041
[9]  
GOATHAM JI, 1969, SAE690387 PAP
[10]   UNSTEADY-FLOW IN A SUPERSONIC CASCADE WITH STRONG IN-PASSAGE SHOCKS [J].
GOLDSTEIN, ME ;
BRAUN, W ;
ADAMCZYK, JJ .
JOURNAL OF FLUID MECHANICS, 1977, 83 (DEC) :569-604