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Experimental investigation of the effects of plastic flow in a tension panel with a circular hole /

Seven uniformly dimensioned 24S-T tension panels with a central circular hole were subjected to various loads in order to study the effects of plastic flow at the point of maximum stress concentration. The results, presented in graphical form, show that, as the amount of plastic flow increases, the...

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Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Griffith, George E. (Autor)
Autor Corporativo: United States. National Advisory Committee for Aeronautics
Formato: Documento de Gobierno Electrónico eBook
Idioma:Inglés
Publicado: Washington, D.C. : National Advisory Committee for Aeronautics, 1948.
Colección:Technical note (United States. National Advisory Committee for Aeronautics) ; no. 1705.
Temas:
Acceso en línea:Texto completo

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