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.

Détails bibliographiques
Cote:Libro Electrónico
Auteur principal: Boughan, Rolla B.
Collectivités auteurs: United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
Autres auteurs: Baab, George W.
Format: Électronique eBook
Langue:Inglés
Publié: Washington, D.C. : National Advisory Committee for Aeronautics, [1944]
Collection:Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L204.
Sujets:
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.
Accès en ligne:Texto completo
Description
Résumé: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.
Description: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.
Description matérielle:1 online resource (8, [6] pages) : illustrations
Bibliographie:Includes bibliographical references.
ISBN:9781680156492
1680156497

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