Critical combinations of shear and direct axial stress for curved rectangular panels /

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A solution is presented for the problem of the buckling of curved rectangular panels subjected to combinded shear and direct axial stress. Charts giving theoretical critical combinations of shear and direct axial stress are presented for panels having five different length-width ratios.

Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Schildcrout, Murry
Autor Corporativo: United States. National Advisory Committee for Aeronautics
Otros Autores: Stein, Manuel
Formato: Documento de Gobierno Electrónico eBook
Idioma:Inglés
Publicado: Washington, D.C. : National Advisory Committee for Aeronautics, 1949.
Colección:Technical note (United States. National Advisory Committee for Aeronautics) ; no. 1928.
Temas:
Plates (Engineering)
Curvature.
Buckling (Mechanics)
Shear (Mechanics)
Strains and stresses.
Plaques (Ingénierie)
Courbure.
Flambage (Résistance des matériaux)
Cisaillement (Mécanique)
Contraintes (Mécanique)
shear stress.
Acceso en línea:Texto completo
Descripción
Sumario:A solution is presented for the problem of the buckling of curved rectangular panels subjected to combinded shear and direct axial stress. Charts giving theoretical critical combinations of shear and direct axial stress are presented for panels having five different length-width ratios.
Because the actual critical compressive stress of rectangular panels having substantial curvature is known to be much lower than the theoretical value, a semi-empirical method of analysis of curved panels subjected to combined shear and direct axial stress is presented for use in design.
Notas:"August 1949."
NACA TN No. 1928.
Descripción Física:1 online resource (29 pages) : illustrations
Bibliografía:Includes bibliographical references.
ISBN:9781680156164
1680156160

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