Residual strength prediction for aircraft panels with multiple site damage, using the ''EPFEAM'' for stable crack growth analysis (Q1898444)
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scientific article; zbMATH DE number 797292
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Residual strength prediction for aircraft panels with multiple site damage, using the ''EPFEAM'' for stable crack growth analysis |
scientific article; zbMATH DE number 797292 |
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Residual strength prediction for aircraft panels with multiple site damage, using the ''EPFEAM'' for stable crack growth analysis (English)
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29 October 1995
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