紀要論文 小型航空機の設計試作に関する研究:主翼構造と応力状態の測定と評価

正岡, 大武

内容記述
This study is conducted as a part of prototype design of a new category small aircraft in our laboratory. In the present study, the stress acting on the main wing structure of a new category small aircraft during cruise is calculated and compared with the result of stress-strain experiment acting on 1:1 scale model of the main wing in order to verify the validity. In addition, reevaluating the main wing structure, optimization of the prototype design was attempted.Key Words : Light Sport Aircraft, Stress- strain experiment, Main wing structure
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https://hosei.repo.nii.ac.jp/?action=repository_action_common_download&item_id=14129&item_no=1&attribute_id=22&file_no=1

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