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BS EN 4247:2005
Aerospace series. Aluminium alloy AL-P2024-T42. Plate. 6 mm <a =140 mm
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Summary
Proof stress;Sheet materials;Air transport engineering;Chemical composition;Dimensions;Aluminium alloys;Aircraft components;Heat treatment;Tensile strength;Aluminium;Elongation
Technical characteristics
| Publisher | British Standards Institution (BSI) |
| Publication Date | 10/04/2005 |
| Page Count | 10 |
| Themes | Elongation |
| EAN | --- |
| ISBN | --- |
| Weight (in grams) | --- |
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04/10/2005
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