BUCKLING AND LATERAL VIBRATION OF RECTANGULAR PLATES SUBJECT TO INPLANE LOADS - RITZ APPROACH

被引:52
作者
BASSILY, SF
DICKINSON, SM
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D O I
10.1016/0022-460X(72)90951-0
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
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页码:219 / +
页数:1
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共 13 条
[1]  
BATDORF SB, 1947, LANGLEY MEMORIAL AER
[2]  
BAZLEY NW, 1965, TG626 JOHNS HOPK U A
[3]  
BUDIANSKY B, 1948, LANGLEY MEMORIAL AER
[4]  
CLAASEN RW, 1960, NAVWEPS7016 REP
[5]   SHEAR BUCKLING OF RECTANGULAR PLATES WITH MIXED BOUNDARY CONDITIONS [J].
COOK, IT ;
ROCKEY, KC .
AERONAUTICAL QUARTERLY, 1963, 14 (04) :349-356
[6]  
DAWE DJ, 1969, 1062 AER RES C CURR
[7]   LATERAL VIBRATION OF RECTANGULAR PLATES SUBJECT TO IN-PLANE FORCES [J].
DICKINSON, SM .
JOURNAL OF SOUND AND VIBRATION, 1971, 16 (04) :465-+
[8]  
IGUCHI S, 1938, 305 HOKK U FAC ENG M
[9]  
ODMAN STA, 1955, NR24 P SWED CEM CONC, P7
[10]   VIBRATIONS OF RECTANGULAR CANTILEVER PLATES SUBJECTED TO IN-PLANE ACCELERATION LOADS [J].
SIMONS, DA ;
LEISSA, AW .
JOURNAL OF SOUND AND VIBRATION, 1971, 17 (03) :407-&