Flat sheet metal girder with very thin metal web : Part 3 : Sheet metal girders with spars resistant to bending - the stress in uprights - diagonal tension fields /

This report continues the work presented in NACA-TM 605 and expands the scope to include the change in specific number of wrinkles from direction x to z, so that b and f become variable in direction z. Moreover, it seems likely that b and f increase from the edge toward the center if the sheet is in...

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Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Wagner, Herbert, 1900-1982
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, [1931]
Colección:Technical memorandums (United States. National Committee for Aeronautics) ; no. 606.
Temas:
Sheet-metal.
Girders.
Mathematics.
Struts (Engineering)
Strains and stresses.
Bending.
Tôle.
Poutres.
Mathématiques.
Étrésillons.
Contraintes (Mécanique)
sheet metal.
mathematics.
applied mathematics.
strain.
stress.
Bending
Girders
Mathematics
Sheet-metal
Strains and stresses
Acceso en línea:Texto completo
Descripción
Sumario:This report continues the work presented in NACA-TM 605 and expands the scope to include the change in specific number of wrinkles from direction x to z, so that b and f become variable in direction z. Moreover, it seems likely that b and f increase from the edge toward the center if the sheet is infinitely thin.
Notas:"February, 1931."
NACA TM No. 606.
Translated from Zeitschrift fur Flugtechnik und Motorluftschiffahrt. Vol. 20, No. 11, pp. 281-284, June 14, and No. 12, pp. 306-314, June 28, 1929, by the National Advisory Committee for Aeronautics.
Descripción Física:1 online resource (39, [8] pages) : illustrations
Bibliografía:Includes bibliographical references.
ISBN:9781680156584
1680156586

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