Stress And Distortion Analysis Of A Swept Box Beam Having Bulkheads Perpendicular To The Spars

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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 example and its results are compared with previously published test data.
Technical Note - National Advisory Committee for Aeronautics

Author: United States. National Advisory Committee for Aeronautics
language: en
Publisher:
Release Date: 1950
Annual Report of the National Advisory Committee for Aeronautics

Author: United States. National Advisory Committee for Aeronautics
language: en
Publisher:
Release Date: 1950