Title of article
Buckling of anisotropic sandwich panels containing holes: Part I - overall buckling
Author/Authors
Hadi، B. K. نويسنده , , Matthews، F. L. نويسنده ,
Issue Information
روزنامه با شماره پیاپی سال 2001
Pages
-204
From page
205
To page
0
Abstract
This paper presents a method for calculating the overall buckling load of simply supported composite sandwich panels containing a hole. Both the pre-buckling analysis and the overall buckling results are compared with other predictions and with experimental data where available. Good agreement is found if the hole diameter is less than 30% of the plate width.
Keywords
Delamination , prediction , Experiment , Sublaminate , Damage tolerance
Journal title
COMPOSITE STRUCTURES
Serial Year
2001
Journal title
COMPOSITE STRUCTURES
Record number
3800
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