Title of article
Interval Analysis Method on the Buckling of Composite Laminate
Author/Authors
QIU، نويسنده , , Zhi-ping and LI، نويسنده , , Fei and YANG، نويسنده , , Jia-ling، نويسنده ,
Issue Information
روزنامه با شماره پیاپی سال 2005
Pages
5
From page
218
To page
222
Abstract
A method named interval analysis method, which solves the buckling load of composite laminate with uncertainties, is presented. Based on interval mathematics and Taylor series expansion, the interval analysis method is used to deal with uncertainties. Not necessarily knowing the probabilistic statistics characteristics of the uncertain variables, only little information on physical properties of material is needed in the interval analysis method, that is, the upper bound and lower bound of the uncertain variable. So the interval of response of the structure can be gotten through less computational efforts. The interval analysis method is efficient under the condition that probability approach cannot work well because of small samples and deficient statistics characteristics. For buckling load of a special cross-ply laminates and antisymmetric angle-ply laminates with all edges simply supported, calculations and comparisons between interval analysis method and probability method are performed.
Keywords
Buckling load , Uncertain parameter , probabilistic statistics method , Interval Analysis , Laminate
Journal title
Chinese Journal of Aeronautics
Serial Year
2005
Journal title
Chinese Journal of Aeronautics
Record number
2264533
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