書誌事項
- タイトル別名
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- Development of Corrugated Morphing Wing and Its Driving Demonstration in the Wind Tunnel Test
- コルゲートガタ モーフィングヨク ノ カイハツ ト フウドウ シケン ニ オケル クドウ ジッショウ
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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.
収録刊行物
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- 日本航空宇宙学会論文集
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日本航空宇宙学会論文集 61 (5), 133-140, 2013
一般社団法人 日本航空宇宙学会
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詳細情報 詳細情報について
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- CRID
- 1390001204469085952
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- NII論文ID
- 130003382933
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- NII書誌ID
- AA11307372
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- ISSN
- 24323691
- 13446460
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- NDL書誌ID
- 024931663
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- 本文言語コード
- ja
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- データソース種別
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- JaLC
- NDL
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- CiNii Articles
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- 抄録ライセンスフラグ
- 使用不可