Aeronautical Research Institute, University of Tokyo
雑誌名
東京大學航空研究所報告
雑誌名(英)
Report/Aeronautical Research Institute, University of Tokyo
巻
25
号
7
ページ
149 - 159
発行年
1959-07
抄録（英）
An approximate solution is presented to obtain the static stress distributions in a swept-back box-beam having asymmetrical section. The box-beam is assumed to consist of four concentrated flanges of different cross-sectional area and four thin walls of different thickness, which connect the flanges. The ribs are assumed perfectly stiff except the one nearest to the root.
The Stress Distribution in a Swept-back Box-beam under Torsional and Bending Loads
SA2404815.pdf
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