FLUTTER OF RECTANGULAR SIMPLY SUPPORTED PANELS AT HIGH SUPERSONIC SPEEDS

被引:84
作者
HEDGEPETH, JM
机构
来源
JOURNAL OF THE AERONAUTICAL SCIENCES | 1957年 / 24卷 / 08期
关键词
D O I
10.2514/8.3908
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:563 / &
相关论文
共 31 条
[1]   PISTON THEORY - A NEW AERODYNAMIC TOOL FOR THE AEROELASTICIAN [J].
ASHLEY, H ;
ZARTARIAN, G .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1956, 23 (12) :1109-1118
[2]  
Bisplinghoff R. L., 1956, VIBRATIONS THERMALLY
[3]  
EISLEY JG, 1955, GALCIT OSRTN55236 RE
[4]  
EISLEY JG, 1956, GALCIT OSRTN56296 RE
[5]  
EVVARD JC, 1950, NACA REPORT, V951
[6]   THE STATIC STABILITY OF A 2-DIMENSIONAL CURVED PANEL IN A SUPERSONIC FLOW, WITH AN APPLICATION TO PANEL FLUTTER [J].
FUNG, YC .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1954, 21 (08) :556-565
[7]  
FUNG YC, 1955, GALCIT OSRTN55237 RE
[8]   AN EXACT SOLUTION FOR 2-DIMENSIONAL LINEAR PANEL FLUTTER AT SUPERSONIC SPEEDS [J].
GOLAND, M ;
LUKE, YL .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1954, 21 (04) :275-276
[9]  
GOLAND M, 1954, J AERONAUTICAL SCI, V21, P276
[10]  
HAYES WD, 1950, AL1029 N AM AV REP