Stress and distortion analysis of a swept box beam having bulkheads perpendicular to the spars /

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 examp...

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Bibliographic Details
Main Author: Heldenfels, Richard R. (Author)
Corporate Authors: United States. National Advisory Committee for Aeronautics, Knovel (Firm)
Other Authors: Zender, George W., Libove, Charles
Format: Government Document Electronic eBook
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1950.
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; no. 2232.
Subjects:
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