ON PANEL FLUTTER IN THE PRESENCE OF A BOUNDARY LAYER

被引:22
作者
MILES, JW
机构
来源
JOURNAL OF THE AEROSPACE SCIENCES | 1959年 / 26卷 / 02期
关键词
D O I
10.2514/8.7949
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
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页码:81 / &
相关论文
共 12 条
[1]  
LEES L, 1947, NACA TN1360
[2]  
LEES L, 1946, NACA TN1115, P67
[4]  
Lin CC., 1955, THEORY HYDRODYNAMIC
[5]   ON THE AERODYNAMIC INSTABILITY OF THIN PANELS [J].
MILES, JW .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1956, 23 (08) :771-780
[6]   ON THE GENERATION OF SURFACE WAVES BY SHEAR FLOWS [J].
MILES, JW .
JOURNAL OF FLUID MECHANICS, 1957, 3 (02) :185-204
[7]   SUPERSONIC FLUTTER OF A CYLINDRICAL SHELL .2. [J].
MILES, JW .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1958, 25 (05) :312-316
[8]   SUPERSONIC FLUTTER OF A CYLINDRICAL SHELL [J].
MILES, JW .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1957, 24 (02) :107-118
[9]  
MILES JW, 1956, GMTR32 RAM CORP REP
[10]  
MILES JW, 1955, AM52A RAM CORP REP