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The stability under longitudinal compression of flat symmetric corrugated-core sandwich plates with simply supported loaded edges and simply supported or clamped unloaded edges /
A theory for the elastic behavior of orthotropic sandwich plates is used to determine the compressive buckling-load parameters of flat symmetrical corrugated core sandwich plates with simply supported loaded edges and simply supported or clamped unloaded edges.
| Cote: | Libro Electrónico |
|---|---|
| Auteur principal: | |
| Collectivités auteurs: | , |
| Format: | Publication officielle Électronique eBook |
| Langue: | Inglés |
| Publié: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1952.
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| Collection: | Technical note (United States. National Advisory Committee for Aeronautics) ;
no. 2679. |
| Sujets: | |
| Accès en ligne: | Texto completo |