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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.
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Stress and distortion analysis of a swept box beam having bulkheads perpendicular to the spars
1950, National Advisory Committee for Aeronautics
in English
1680156187 9781680156188
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Edition Notes
Date of issue: November 1950.
Report no. NACA-TN-2232
Includes bibliographical references.
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