Title The strength and stiffness of shear webs with and without lightening holes / Paul Kuhn

Published Washington, D.C. : National Advisory Committee for Aeronautics, [1942]

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Description 1 online resource (29 pages, 15 unnumbered pages) : illustrations Series Wartime Report / National Advisory Committee for Aeronautics ; number L402 Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L402 Summary Nearly 200 tests were made on the strength of shear webs of 24S-T aluminum alloy, with and without lightening holes. The tests were made in a jig of the single-specimen type, in which the specimen is free to collapse completely without developing diagonal tension. The lightening holes were circular and had either flanged edges or beaded edges, the specimens with flanged edges constituting by far the largest test group Notes NACA Wartime Report L-402 Originally issued as NACA as an Advance Restricted Report (June 1942) Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia Bibliography Includes bibliographical references Notes Print version record Subject Aluminum alloys. Holes. Shear (Mechanics) Strength of materials. Strains and stresses. Monocoque construction. Charts, diagrams, etc. aluminum alloy. shear stress. strength of materials. stress. strain. diagrams. Aluminum alloys Charts, diagrams, etc. Holes Monocoque construction Shear (Mechanics) Strains and stresses Strength of materials Form Electronic book Author United States. National Advisory Committee for Aeronautics. Langley Aeronautical Laboratory. ISBN 9781680156539 1680156535

Other Titles NACA Wartime Reports. Series L

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