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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.
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Subjects
Aluminum alloys, Plates (Engineering), Strains and stresses, Buckling (Mechanics), Airplanes, Materials, Charts, diagrams, Aluminium, Alliages, Plaques (Ingénierie), Contraintes (Mécanique), Flambage (Résistance des matériaux), Avions, Matériaux, Tableaux, graphiques, Aluminum alloy, Stress, Strain, Buckling, Warping, DiagramsShowing 1 featured edition. View all 1 editions?
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Charts for calculation of the critical compressive stress for local instability of idealized web- and T-stiffened panels
1944, National Advisory Committee for Aeronautics
in English
1680156497 9781680156492
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Edition Notes
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.
Includes bibliographical references.
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