SHEAR BUCKLING OF RECTANGULAR PLATES WITH MIXED BOUNDARY CONDITIONS

被引：26

作者：

COOK, IT

ROCKEY, KC

机构：

来源：

AERONAUTICAL QUARTERLY | 1963年 / 14卷 / 04期

关键词：

D O I：

10.1017/S0001925900002900

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：349 / 356

页数：8

共 11 条

[1] BUDIANSKY B, 1948, NACA TN1559
[2] SHEAR BUCKLING OF CLAMPED AND SIMPLY-SUPPORTED INFINITELY LONG PLATES REINFORCED BY CLOSED-SECTION TRANSVERSE STIFFENERS
COOK, IT
ROCKEY, KC
[J]. AERONAUTICAL QUARTERLY, 1962, 13 (03): : 212 - 222
[3] SHEAR BUCKLING OF CLAMPED AND SIMPLY-SUPPORTED INFINITELY LONG PLATES REINFORCED BY TRANSVERSE STIFFENERS
COOK, IT
ROCKEY, KC
[J]. AERONAUTICAL QUARTERLY, 1962, 13 (01): : 41 - 70
[4] IGUCHI S, 1938, INGENIEUR ARCH 9, P1
[5] LEGGETT MA, 1941, RM1991
[6] MOHEIT W, 1939, THESIS TH DARMSTADT
[7] SHEAR BUCKLING OF CLAMPED AND SIMPLY-SUPPORTED INFINITELY LONG PLATES REINFORCED BY TRANSVERSE STIFFENERS AND A CENTRAL LONGITUDINAL STIFFENER
ROCKEY, KC
COOK, IT
[J]. AERONAUTICAL QUARTERLY, 1962, 13 (02): : 95 - 114
[8] SKAN SW, 1924, P ROY SOC LONDON S A, V105, P582
[9] STEIN M, 1947, NACA TN1222
[10] STOWELL EZ, 1943, NACA WR L476