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Results are presented of tests of two sets of 20 curved-sheet specimens to determine the effect of normal pressure on the critical compressive and shear stress of curved sheet. It was found that normal pressure raised the critical compressive and shear stress of curved sheet except when outward bulging occurred in compression, in which case the critical stress was lowered by normal pressure.
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Subjects
Box beams, Aluminum alloys, Plates (Engineering), Curvature, Loads (Mechanics), Shear (Mechanics), Buckling (Mechanics), Strains and stresses, Charts, diagrams, Poutres-caissons, Aluminium, Alliages, Charges, Cisaillement (Mécanique), Flambage (Résistance des matériaux), Contraintes (Mécanique), Tableaux, graphiques, Aluminum alloy, Shear stress, Warping, Buckling, Stress, Strain, DiagramsShowing 1 featured edition. View all 1 editions?
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Effect of normal pressure on the critical compressive and shear stress of curved sheet
1945, National Advisory Committee for Aeronautics
in English
1680156357 9781680156355
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Edition Notes
NACA Wartime Report L-57.
Originally issued as NACA as Advance Restricted Report L5B10 (March 1945).
Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia.
Includes bibliographical references.
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