コルゲート型モーフィング翼の開発と風洞試験における駆動実証

• 資料種別: 記事
• タイトル: コルゲート型モーフィング翼の開発と風洞試験における駆動実証
• 著者・編者: 杉浦 綾; 横関 智弘; 平野 義鎭
• 著者標目: 杉浦 綾; 横関 智弘; 平野 義鎭
• 並列タイトル等: Development of Corrugated Morphine Wing and Its Driving Demonstration in the Wind Tunnel Test
• タイトル（掲載誌）: 日本航空宇宙学会論文集 = Journal of the Japan Society for Aeronautical and Space Sciences
• 巻号年月日等（掲載誌）: 61(5):2013.10
• 掲載巻: 61
• 掲載号: 5
• 掲載ページ: 133-140
• 掲載年月日（W3CDTF）: 2013-10
• ISSN（掲載誌）: 1344-6460
• ISSN-L（掲載誌）: 1344-6460
• 出版事項（掲載誌）: 東京 : 日本航空宇宙学会
• 出版地（国名コード）: JP
• 本文の言語コード: jpn
• 件名標目: Morphine Wing; Structural Design; Smart Structure; Wind Tunnel Test
• NDLC: ZN25
• 対象利用者: 一般
• 所蔵機関: 国立国会図書館
• 請求記号: Z74-B503
• 連携機関・データベース: 国立国会図書館 : 国立国会図書館雑誌記事索引; https://ndlsearch.ndl.go.jp
• 書誌ID（NDLBibID）: 024931663; http://id.ndl.go.jp/bib/024931663
• 整理区分コード: 632

• 要約等: This paper describes the development and the wind tunnel test of a variable geometry morphing airfoil using corrugated structures. Feasibility of a morphing wing with corrugated flexible seamless flap-like structure is verified by the finite element analysis, and a prototype is manufactured using carbon fiber reinforced plastics. For the actuation system, two servomotors are installed inside the prototype wing to control the airfoil shape by the chord-wise tension of the connected wires. Successful actuation of the prototype wing is demonstrated under the air speed up to 30m/s in the wind tunnel test. Basic aerodynamic properties are also evaluated in comparison to traditional airfoil with a hinged control surface. Lift increase of variable corrugated wing is recognized when the flap angle increases.
• DOI: 10.2322/jjsass.61.133
• オンライン閲覧公開範囲: インターネット公開
• 連携機関・データベース: 科学技術振興機構 : J-STAGE; http://www.jstage.jst.go.jp

• 要約等: This paper describes the development and the wind tunnel test of a variable geometry morphing airfoil using corrugated structures. Feasibility of a morphing wing with corrugated flexible seamless flap-like structure is verified by the finite element analysis, and a prototype is manufactured using carbon fiber reinforced plastics. For the actuation system, two servomotors are installed inside the prototype wing to control the airfoil shape by the chord-wise tension of the connected wires. Successful actuation of the prototype wing is demonstrated under the air speed up to 30m/s in the wind tunnel test. Basic aerodynamic properties are also evaluated in comparison to traditional airfoil with a hinged control surface. Lift increase of variable corrugated wing is recognized when the flap angle increases.
• DOI: 10.2322/jjsass.61.133; https://doi.org/10.2322/jjsass.61.133
• 関連情報（URI）: http://id.ndl.go.jp/bib/024931663; https://ndlsearch.ndl.go.jp/books/R000000004-I024931663; https://www.jstage.jst.go.jp/article/jjsass/61/5/61_61_133/_pdf
• 参照: Composite corrugated structures for morphing wing skin applications; https://cir.nii.ac.jp/crid/1361137046407083008; Aircraft Structural Morphing Using Tendon Actuated Compliant Cellular Trusses; https://cir.nii.ac.jp/crid/1361137046410811008; Development and Flight Testing of a Morphing Aircraft, the NextGen MFX-1; https://cir.nii.ac.jp/crid/1361981469387626496; The Aircraft Morphing Program; https://cir.nii.ac.jp/crid/1362262946133151232; Multi-Functional Morphing Trailing Edge for Control of All-Composite, All-Electric Flying Wing Aircraft; https://cir.nii.ac.jp/crid/1362544419545890560; A novel unmanned aircraft with solid-state control surfaces: Analysis and flight demonstration; https://cir.nii.ac.jp/crid/1362544419850156416; Flight Testing of Mission Adaptive Compliant Wing; https://cir.nii.ac.jp/crid/1363107369821186176
• 連携機関・データベース: 国立情報学研究所 : CiNii Research; https://cir.nii.ac.jp/
• 提供元機関・データベース: Japan Link Center; https://japanlinkcenter.org/top; 雑誌記事索引データベース; https://ndlsearch.ndl.go.jp; Crossref; https://www.crossref.org; CiNii Articles
• 書誌ID（NDLBibID）: 024931663; http://id.ndl.go.jp/bib/024931663
• NII論文ID: 130003382933