CRITICAL BUCKLING OF SOME STIFFENED PANELS IN COMPRESSION, SHEAR AND BENDING

被引：15

作者：

PLANK, RJ ^{[1
]}

WILLIAMS, FW ^{[1
]}

机构：

[1] UNIV BIRMINGHAM,DEPT CIVIL ENGN,BIRMINGHAM,ENGLAND

来源：

AERONAUTICAL QUARTERLY | 1974年 / 25卷 / AUG期

关键词：

D O I：

10.1017/S0001925900006958

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：165 / 179

页数：15

共 50 条

[1] CRITICAL BUCKLING OF SOME STIFFENED PANELS IN COMPRESSION, SHEAR AND BENDING.
Plank, R.J.
Williams, F.W.
1974, 25 (Part 3): : 165 - 179
[2] BUCKLING, POSTBUCKLING, AND FAILURE OF STIFFENED PANELS UNDER SHEAR AND COMPRESSION
ARNOLD, RR
PAREKH, JC
JOURNAL OF AIRCRAFT, 1987, 24 (11): : 803 - 811
[3] NUMERICAL RESULTS FOR INITIAL BUCKLING OF SOME STIFFENED PANELS IN COMPRESSION
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WITTRICK, WH
AERONAUTICAL QUARTERLY, 1972, 23 (FEB): : 24 - &
[4] BUCKLING ANALYSIS OF DISCRETELY STIFFENED COMPOSITE CURVED PANELS UNDER COMPRESSION AND SHEAR
童贤鑫
B.Geier
K.Rohwer
AppliedMathematicsandMechanics(EnglishEdition), 1986, (04) : 315 - 326
[5] Cyclic Buckling Tests Under Combined Compression and Shear on Composite Stiffened Panels
Cordisco, P.
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AIAA JOURNAL, 2009, 47 (12) : 2879 - 2893
[6] BUCKLING OF LONGITUDINALLY STIFFENED PLATES IN BENDING AND COMPRESSION
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[7] A FINITE STRIP ANALYSIS OF THE BUCKLING CHARACTERISTICS OF SOME COMPOSITE STIFFENED SHEAR PANELS
LOUGHLAN, J
COMPOSITE STRUCTURES, 1994, 27 (03) : 283 - 294
[8] A UNIFIED APPROACH TO INITIAL BUCKLING OF STIFFENED PANELS IN COMPRESSION
WITTRICK, WH
AERONAUTICAL QUARTERLY, 1968, 19 : 265 - &
[9] REPEATED BUCKLING TESTS OF STIFFENED THIN SHEAR PANELS
ARIGUR, J
SINGER, J
LIBAI, A
ISRAEL JOURNAL OF TECHNOLOGY, 1982, 20 (4-5): : 220 - 231
[10] DURABILITY UNDER REPEATED BUCKLING OF STIFFENED SHEAR PANELS
WELLER, T
KOLLET, M
LIBAI, A
SINGER, J
JOURNAL OF AIRCRAFT, 1987, 24 (01): : 6 - 7

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