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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.

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

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