Title Stress and distortion analysis of a swept box beam having bulkheads perpendicular to the spars / by Richard R. Heldenfels, George W. Zender, and Charles Libove

Published Washington, D.C. : National Advisory Committee for Aeronautics, 1950

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Description 1 online resource (90 pages) : illustrations Series National Advisory Committee for Aeronautics ; no. 2232 Technical note (United States. National Advisory Committee for Aeronautics) ; no. 2232. Summary A method is presented for the approximate calculation of the stresses and distortions in a box beam representing the main structural component of a swept wing with a carry-through section and with bulkheads perpendicular to the spars. The application of the method is illustrated by a numerical example and its results are compared with previously published test data Notes Date of issue: November 1950 Report no. NACA-TN-2232 Bibliography Includes bibliographical references Notes Print version record Subject Box beams. Bulkheads. Strains and stresses. Structural analysis (Engineering) box beams. structural analysis. Box beams Bulkheads Strains and stresses Structural analysis (Engineering) Form Electronic book Author Zender, George W Libove, Charles United States. National Advisory Committee for Aeronautics. ISBN 9781680156188 1680156187

OTHER TI Technical Report Archive & Image Library (TRAIL)

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