Critical combinations of shear and longitudinal direct stress for long plates with transverse curvature /

A theoretical solution is presented for the buckling stresses of long plates with transverse curvature loaded in shear and longitudinal direct stress. The theoretical critical-stress combinations for plates having either simply supported or clamped edges are given in figures and tables and a compari...

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Detalles Bibliográficos
Clasificación:Libro Electrónico
Autores principales: Batdorf, S. B. (Autor), Schildcrout, Murry (Autor), Stein, Manuel (Autor)
Autor Corporativo: Langley Aeronautical Laboratory
Formato: Documento de Gobierno Electrónico eBook
Idioma:Inglés
Publicado: Washington, D.C. : National Advisory Committee for Aeronautics, 1947.
Colección:Technical note (United States. National Advisory Committee for Aeronautics) ; no. 1347.
Temas:
Plates (Engineering)
Strains and stresses.
Buckling (Mechanics)
Loads (Mechanics)
Shear (Mechanics)
Plaques (Ingénierie)
Contraintes (Mécanique)
Flambage (Résistance des matériaux)
Charges.
Cisaillement (Mécanique)
stress.
strain.
warping.
buckling.
shear stress.
Strains and stresses
Acceso en línea:Texto completo
Descripción
Sumario:A theoretical solution is presented for the buckling stresses of long plates with transverse curvature loaded in shear and longitudinal direct stress. The theoretical critical-stress combinations for plates having either simply supported or clamped edges are given in figures and tables and a comparison is made with a previous theoretical solution for simply supported plates.
Notas:"Langley Memorial Aeronautical Laboratory."
Date of issue: June 1947.
Report no. NACA TN No. 1347.
Descripción Física:1 online resource (27 pages, 9 unnumbered pages) : illustrations, tables
Bibliografía:Includes bibliographical references (pages 23-24)
ISBN:9781680156065
1680156063

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