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 |
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Elsevier Ltd
01-05-2001
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| Abstract | 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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| AbstractList | 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. |
| Author | Prusty, B.G Ray, C Satsangi, S.K |
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| Title | Corrigendum to “First ply failure analysis of stiffened panels – a finite element approach” [Composite Structures, 51 (2001) 73–81] |
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