A DETERMINISTIC METHOD TO PREDICT THE EFFECT OF UNKNOWN-BUT-BOUNDED ELASTIC-MODULI ON THE BUCKLING OF COMPOSITE STRUCTURES

被引：41

作者：

ELISHAKOFF, I

LI, YW

STARNES, JH

机构：

[1] FLORIDA ATLANTIC UNIV,DEPT MECH ENGN,BOCA RATON,FL 33431

[2] NASA,LANGLEY RES CTR,HAMPTON,VA 23664

来源：

COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING | 1994年 / 111卷 / 1-2期

关键词：

D O I：

10.1016/0045-7825(94)90043-4

中图分类号：

T [工业技术];

学科分类号：

08 ;

摘要：

A new, non-probabilistic method is developed in this study to predict the variability in buckling loads of composite plates and shells stemming from the unavoidable scatter in elastic moduli. The available measurements of elastic moduli are fitted by the four-dimensional uncertainty 'box' and appropriate ellipsoid. For the specific cases considered, the maximum buckling load of the composite plate exceeds by 11% the value of the buckling load based on the calculation using the nominal values of elastic moduli. In the case of the cylindrical shell, an appropriate exceedance constitutes 9%.

引用

页码：155 / 167

页数：13

共 9 条

[1] ELASTIC-CONSTANTS OF CARBON-FIBER COMPOSITES [J].

GOGGIN, PR .

JOURNAL OF MATERIALS SCIENCE, 1973, 8 (02) :233-244

[2] BUCKLING OF ANGLE-PLY LAMINATED CIRCULAR CYLINDRICAL-SHELLS [J].

HIRANO, Y .

JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME, 1979, 46 (01) :233-234

[3]

Jones R. M, 1975, MECH COMPOS MATER, P45

[4]

TEWARY VK, 1978, MECHANICS FIBER COMP, P108

[5]

TINOSHENKO SP, 1961, THEORY ELASTIC STABI, P462

[6]

VINSON JR, 1986, BEHAV STRUCTURES COM, P63

[7]

WHITNEY JM, 1987, STRUCTURAL ANAL LAMI, P151

[8]

[No title captured]

[9]

1987, ENG MATERIALS HDB, V1, P445

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