Effect of normal pressure on the critical compressive stress of curved sheet /

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Results are presented of tests of two specimens tested to study the effect of normal pressure on the critical compressive stress for thin curved sheets. These specimens are designated by their respective rib spacings of 10 inches and 30 inches. The relationship between compressive stress and normal...

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Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Rafel, Norman
Autores Corporativos: United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
Formato: Electrónico eBook
Idioma:Inglés
Publicado: Washington, D.C. : National Advisory Committee for Aeronautics, [1942]
Colección:Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L258.
Temas:
Atmospheric pressure.
Buckling (Mechanics)
Strains and stresses.
Loads (Mechanics)
Charts, diagrams, etc.
Pression atmosphérique.
Flambage (Résistance des matériaux)
Contraintes (Mécanique)
Charges.
Tableaux, graphiques, etc.
atmospheric pressure.
buckling.
warping.
stress.
strain.
diagrams.
Atmospheric pressure
Strains and stresses
Acceso en línea:Texto completo
Descripción
Sumario:Results are presented of tests of two specimens tested to study the effect of normal pressure on the critical compressive stress for thin curved sheets. These specimens are designated by their respective rib spacings of 10 inches and 30 inches. The relationship between compressive stress and normal pressure at which buckles disappeared is independent of whether the buckles were made to disappear by increase of normal pressure or decrease of compressive stress.
Notas:NACA Wartime Report L-258.
Originally issued as NACA as a Restricted Bulletin (November 1942).
Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia.
Descripción Física:1 online resource (2, [8] pages) : illustrations
ISBN:9781680156348
1680156349

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