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A Method of calculating the compressive strength of Z-stiffened panels that develop local instability /
A method, based on the elastic theory for plate buckling and test results for 24S-T aluminum-alloy Z-stiffened panels, is shown for calculating the compressive strength of Z-stiffened panels that develop local instability. This method can be used to calculate the critical compressive stress above, a...
| Cote: | Libro Electrónico |
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| Format: | Publication officielle Électronique eBook |
| Langue: | Inglés |
| Publié: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1947.
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| Collection: | Technical note (United States. National Advisory Committee for Aeronautics) ;
no. 1482. |
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| Accès en ligne: | Texto completo |