Tables of stiffness and carry-over factor for flat rectangular plates under compression /

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Tables of stiffness and carry-over factor are presented for infinitely long flat plates subjected to a uniformly distributed longitudinal compressive load. The tables are intended for use in solving problems in the stability of structures composed of plates under compression.

Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Kroll, W. D.
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, [1943]
Colección:Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L398.
Temas:
Plates (Engineering)
Axial loads.
Loads (Mechanics)
Buckling (Mechanics)
Stability.
Plaques (Ingénierie)
Charges axiales.
Charges.
Flambage (Résistance des matériaux)
Stabilité.
axial loads.
warping.
buckling.
stability.
Axial loads
Stability
Acceso en línea:Texto completo
Descripción
Sumario:Tables of stiffness and carry-over factor are presented for infinitely long flat plates subjected to a uniformly distributed longitudinal compressive load. The tables are intended for use in solving problems in the stability of structures composed of plates under compression.
Notas:NACA Wartime Report L-398.
Originally issued as NACA as Advance Restricted Report L3K27 (November 1943).
Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia.
Descripción Física:1 online resource (47 pages) : tables
Bibliografía:Includes bibliographical references.
ISBN:9781680156515
1680156519

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