http://www.loc.gov/mods/v3 http://www.loc.gov/standards/mods/v3/mods-3-2.xsd
Stress and distortion analysis of a swept box beam having bulkheads perpendicular to the spars
National Advisory Committee for Aeronautics.
1 online resource (90 pages) : illustrations
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.
by Richard R. Heldenfels, George W. Zender, and Charles Libove.
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Technical note (United States. National Advisory Committee for Aeronautics) ; no. 2232