Art
J-GLOBAL ID:201802251683026660   Reference number:18A1010520

Wind Tunnel Test of Morphing Flap Driven by Shape Memory Alloy Wires

形状記憶合金ワイヤによるモーフィングフラップの風洞実験
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Material:
Volume: 15  Issue: APISAT-2016  Page: a75-a82(J-STAGE)  Publication year: 2017 
JST Material Number: U0121A  ISSN: 1884-0485  Document type: Article
Article type: 原著論文  Country of issue: Japan (JPN)  Language: ENGLISH (EN)
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Wind tunnel,various testing devices attachment deuices 
Reference (15):
  • 1) American Airlines, Inc.: Annual Reports 2016 Form 10-K, http://phx.corporate-ir.net/External.File?item=UGFyZW50SUQ9NjYxODc4fENoaWxkSUQ9MzY5MDIwfFR5cGU9MQ==&t=1\n (accessed May 3, 2017).
  • 2) Delta Air Lines, Inc.: Delta Air Lines Announces December Quarter and Full Year 2016 Profit, http://s1.q4cdn.com/231238688/files/earnings/2016/4Q/Delta-Air-Lines-Announces-December-Quarter-and-Full-Year-2016-Profit.pdf (accessed May 3, 2017).
  • 3) Bolonkin, A. and Gilyard, G. B.: Estimated Benefits of Variable-geometry Wing Camber Control for Transport Aircraft, NASA TM-1999-206586, 1999.
  • 4) Hisano, M.: Low- noise and high-efficiency technologies of BOEING 787, the Journal of Aviation Environment Research, 16 (2012), pp. 47-52. (in Japanese)
  • 5) Reckzeh, D.: Multifunctional Wing Moveables: Design of the A350XWB and the Way toFuture Concepts, Proc. ICAS 2014, ICAS2014_0133, 2014.
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