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.
Clasificación: | Libro Electrónico |
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Autor principal: | |
Autores Corporativos: | , |
Formato: | Documento de Gobierno Electrónico eBook |
Idioma: | Inglés |
Publicado: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1952.
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Colección: | Technical note (United States. National Advisory Committee for Aeronautics) ;
no. 2679. |
Temas: | |
Acceso en línea: | Texto completo |