Tension fields in originally curved, thin sheets during shearing stresses /

The analysis of the stresses in the sheet and stiffeners is predicated upon the direction of the wrinkles, particularly the tensile stresses (principal stresses). This analysis and the calculation of stresses after buckling form the subject of the present article. It includes: 1) metal cylinders wit...

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Detalles Bibliográficos
Clasificación:Libro Electrónico
Autores principales: Wagner, H. (Autor), Ballerstedt, W. (Autor)
Autor Corporativo: United States. National Advisory Commitee for Aeronautics
Formato: Documento de Gobierno Electrónico eBook
Idioma:Inglés
Publicado: Washington, D.C. : National Advisory Commitee for Aeronautics, [1935]
Colección:Technical memorandum (United States. National Advisory Committee for Aeronautics) ; no. 774.
Temas:
Shells (Engineering)
Thin-walled structures.
Curvature.
Shear (Mechanics)
Strains and stresses.
Coques (Ingénierie)
Structures à parois minces.
Courbure.
Cisaillement (Mécanique)
Contraintes (Mécanique)
shell structures.
shear stress.
strain.
stress.
Acceso en línea:Texto completo
Descripción
Sumario:The analysis of the stresses in the sheet and stiffeners is predicated upon the direction of the wrinkles, particularly the tensile stresses (principal stresses). This analysis and the calculation of stresses after buckling form the subject of the present article. It includes: 1) metal cylinders with closely spaced longitudinal stiffeners; 2) metal cylinders with closely spaced transverse rings.
Notas:"August 1935."
NACA TM No. 774.
Translated from Luftfahrtforschung. Vol. 12, No. 2, pp. 70-74, May 16, 1935, by the National Advisory Commitee for Aeronautics.
Descripción Física:1 online resource (11 pages, 2 unnumbered pages) : illustrations
Bibliografía:Includes bibliographical references.
ISBN:9781680156577
1680156578
Acceso:Access restricted to Ryerson students, faculty and staff.

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