Charts for calculation of the critical compressive stress for local instability of idealized web- and T-stiffened panels /

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Charts are presented for the calculation of the critical compressive stress - the stress at which local instability occurs - for idealized web- and T-stiffened panels, and examples of the use of the charts are given.

Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Boughan, Rolla B.
Autores Corporativos: United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
Otros Autores: Baab, George W.
Formato: Electrónico eBook
Idioma:Inglés
Publicado: Washington, D.C. : National Advisory Committee for Aeronautics, [1944]
Colección:Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L204.
Temas:
Aluminum alloys.
Plates (Engineering)
Strains and stresses.
Buckling (Mechanics)
Airplanes > Materials.
Charts, diagrams, etc.
Aluminium > Alliages.
Plaques (Ingénierie)
Contraintes (Mécanique)
Flambage (Résistance des matériaux)
Avions > Matériaux.
Tableaux, graphiques, etc.
aluminum alloy.
stress.
strain.
buckling.
warping.
diagrams.
Acceso en línea:Texto completo
Descripción
Sumario:Charts are presented for the calculation of the critical compressive stress - the stress at which local instability occurs - for idealized web- and T-stiffened panels, and examples of the use of the charts are given.
Notas:NACA Wartime Report L-204.
Originally issued as NACA as Advance Restricted Report L4H29 (August 1944).
Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia.
Descripción Física:1 online resource (8, [6] pages) : illustrations
Bibliografía:Includes bibliographical references.
ISBN:9781680156492
1680156497

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