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Experimental Studies of Vortex Flaps and Vortex Plates Part 1. 0.53m Span 60deg Delta Wing

Experimental Studies of Vortex Flaps and Vortex Plates Part 1. 0.53m Span 60deg Delta Wing
Digital文書・図像類
李家, 賢一, RINOIE, Kenichi航空宇宙技術研究所1992-03Technical Report of National Aerospace Laboratory TR-1140T1140Tp.16-
Other Libraries in Japan
  • Subject Headinglow-speed aerodynamics; delta wing; vortex flap; votex plate; leading-edge separation vortex
  • Note (General)...e leading-edge separation vortex on the flap surface. Use of a...

ボルテックス･フラップ付きデルタ翼の低速空力特性について:後退角60度と70度の比較

ボルテックス･フラップ付きデルタ翼の低速空力特性について:後退角60度と70度の比較
Digital文書・図像類
李家, 賢一, 藤田, 敏美, 岩崎, 昭人, 藤枝, 郭俊, Rinoie, Kenichi, Fujita, Toshimi, Iwasaki, Akihito, Fujieda, Hirotoshi航空宇宙技術研究所1994-07航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1245p.1-13
Other Libraries in Japan
  • Subject Heading...c leading edge separation vortex low speed wind tunnel test su...

Experimental studies of vortex flaps and vortex plates, Part 2: 1.15m span 60 deg delta wing

Experimental studies of vortex flaps and vortex plates, Part 2: 1.15m span 60 deg delta wing
Digital文書・図像類
李家, 賢一, Stollery, L., Rinoie, Kenichi, Stolley, L.航空宇宙技術研究所1992-10航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1180Tp.1-36
Other Libraries in Japan
  • Subject Heading...n leading edge separation vortex control low speed wind tunnel...
  • Note (General)...a leading-edge separation vortex over the flap surface. It was...

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