Corrigendum to “First ply failure analysis of stiffened panels – a finite element approach” [Composite Structures, 51 (2001) 73–81]
The following corrections should be incorporated in Table 2 of the paper: The sequence of laminates in the table should be read as: 1st row - [0 sub 2 /90 sub 2 ] sub s ; 2nd row - [0/90/0/90] sub s ; 3rd row - [0 sub 2 /90] sub s ; 4th row - [0/90] sub s ; p sub 1 and p sub 2 (in the last column) c...
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| Published in: | Composite structures Vol. 52; no. 2; p. 261 |
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| Main Authors: | , , |
| Format: | Journal Article |
| Language: | English |
| Published: |
Elsevier Ltd
01-05-2001
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| Online Access: | Get full text |
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| Summary: | The following corrections should be incorporated in Table 2 of the paper: The sequence of laminates in the table should be read as: 1st row - [0 sub 2 /90 sub 2 ] sub s ; 2nd row - [0/90/0/90] sub s ; 3rd row - [0 sub 2 /90] sub s ; 4th row - [0/90] sub s ; p sub 1 and p sub 2 (in the last column) corresponds to values of Column-4 and 5, respectively. |
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| Bibliography: | ObjectType-Article-2 SourceType-Scholarly Journals-1 ObjectType-Feature-1 content type line 23 |
| ISSN: | 0263-8223 1879-1085 |
| DOI: | 10.1016/S0263-8223(01)00056-3 |