@techreport{oai:jaxa.repo.nii.ac.jp:00044816,
 author = {久能, 和夫 and 伊藤, 誠一 and 岩崎, 和夫 and KUNO, Kazuo and ITO, Seiichi and IWASAKI, Kazuo},
 month = {Feb},
 note = {静的な荷重を受ける主翼構造模型の破壊実験を行い,模型が破壊に至るまでの非線形挙動を追跡した。実験に使用した模型は6個で,後退角のない模型3個と後退角30度の模型2個および後退角45度の模型1個である。実験結果は簡単な計算法による値と比較検討すると共に,詳細な考察を行い,主翼構造設計に役立つ資料とした。, This paper reports on the investigation of the experimental results of the ultimate strength of six wing structures. The six wings, consisting of three non-swept wings, two 30 deg swept wings and one 45 deg swept wing, are designed in order to study the structural efficiency of wing structures, with different structural indices, and the effect of a sweptback angle on the ultimate strength. A procedure for predicting the ultimate strength of a wing structure under a simple loading condition is presented. Comparison of the predicted and the experimental ultimate loads, verifies the usefulness of this procedure., 資料番号: NALTR0562000, レポート番号: NAL TR-562},
 title = {箱型主翼構造模型の破壊実験},
 year = {1979}
}