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
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- Material Type
- 記事
- Author/Editor
- 杉浦 綾横関 智弘平野 義鎭
- Alternative Title
- Development of Corrugated Morphine Wing and Its Driving Demonstration in the Wind Tunnel Test
- Periodical title
- 日本航空宇宙学会論文集 = Journal of the Japan Society for Aeronautical and Space Sciences
- No. or year of volume/issue
- 61(5):2013.10
- Volume
- 61
- Issue
- 5
- Pages
- 133-140
- Publication date of volume/issue (W3CDTF)
- 2013-10
- ISSN (Periodical Title)
- 1344-6460
- ISSN-L (Periodical Title)
- 1344-6460
- Publication (Periodical Title)
- 東京 : 日本航空宇宙学会
- Place of Publication (Country Code)
- JP
- Text Language Code
- jpn
- NDLC
- Target Audience
- 一般
- Holding library
- 国立国会図書館
- Call No.
- Z74-B503
- Data Provider (Database)
- 国立国会図書館 : 国立国会図書館雑誌記事索引
- Bibliographic ID (NDL)
- 024931663
- Bibliographic Record Category (NDL)
- 632
- Summary, etc.
- 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
- Access Restrictions
- インターネット公開
- Data Provider (Database)
- 科学技術振興機構 : J-STAGE
- Summary, etc.
- 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
- Related Material (URI)
- References
- Composite corrugated structures for morphing wing skin applicationsAircraft Structural Morphing Using Tendon Actuated Compliant Cellular TrussesDevelopment and Flight Testing of a Morphing Aircraft, the NextGen MFX-1The Aircraft Morphing ProgramMulti-Functional Morphing Trailing Edge for Control of All-Composite, All-Electric Flying Wing AircraftA novel unmanned aircraft with solid-state control surfaces: Analysis and flight demonstrationFlight Testing of Mission Adaptive Compliant Wing
- Data Provider (Database)
- 国立情報学研究所 : CiNii Research
- Original Data Provider (Database)
- Japan Link Center雑誌記事索引データベースCrossrefCiNii Articles
- Bibliographic ID (NDL)
- 024931663
- NAID
- 130003382933