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Search results 7

Investigation of vortex flaps and other flow control devices on generic high-speed civil transport planforms [microform] / Kevin J. Kjerstad ... [et al.] (NASA/TP ; 1999-209537)

Investigation of vortex flaps and other flow control devices on generic high-speed civil transport planforms [microform] / Kevin J. Kjerstad ... [et al.] (NASA/TP ; 1999-209537)
Microform図書
1999<YCA-NAS 1.60:209537>
National Diet Library
  • Subject HeadingVortex flaps High speed Planforms Subsoni...

An experimental investigation of the confluent boundary layer on a high-lift system [microform] : final project report / by F.O. Thomas and R.C. Nelson

An experimental investigation of the confluent boundary layer on a high-lift system [microform] : final project report / by F.O. Thomas and R.C. Nelson
Microform図書
1997<YCA-NAS 1.26:112979>
National Diet Library
  • Subject Heading...Trailing edges Vortex flaps Flow characteristics Flow co...

超音速航空機(SST)形態の高揚力装置に関する実験的研究

超音速航空機(SST)形態の高揚力装置に関する実験的研究
Digital文書・図像類
郭, 東潤, 宮田, 勝弘, 野口, 正芳, 砂田, 保人, 李家, 賢一, KWAK, Dong-Youn, MIYATA, Katsuhiro, NOGUCHI, Masayoshi, SUNADA, Yasuto, RINOIE, Kenichi航空宇宙技術研究所2002-01航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-14501450p.33-
Other Libraries in Japan
  • Subject HeadingSST, Leading-edge Flap, Vortex Flap, Trailing-edge Flap

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 ...
  • Note (General)...a leading-edge vortex flap at the maximum......of an inverted vortex flap and vortex pla...... the deflected vortex flap without forming a large leadi...

超音速航空機(SST)形態の高揚力装置に関する実験的研究

超音速航空機(SST)形態の高揚力装置に関する実験的研究
Digital文書・図像類
宮田, 勝弘, 李家, 賢一, Kwak, Dong-Youn, 野口, 正芳, Miyata, Katsuhiro, Rinoie, Kenichi, Noguchi, Masayoshi航空宇宙技術研究所2003-05航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1456
Other Libraries in Japan
  • Subject Heading...ow instability vortex flap Reynolds number surface rough...
  • Note (General)...d leading-edge vortex flaps were investig......d leading-edge vortex flaps and the flap ......d leading-edge vortex flaps was obtained,......he non-rounded vortex flaps at a lift coe......d leading-edge vortex flaps were observed changing as th...

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...前縁デバイス 高迎角空気力学 vortex flap delta wing aerodynamics low s...
  • Note (General)...l with tapered vortex flaps to investigat......performance of vortex flaps. The force, s......rns around the vortex flaps at the optimu......over the whole vortex flap surface. 資料番号: AA0004253000 レ...
  • Alternative Title...lta wings with vortex flaps: 60 deg and 70 deg Delta win...

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...分布 離陸上昇時性能 高揚力 vortex flap vortex plate delta wing lift ...
  • Note (General)...out on several vortex flap and vortex pla......icate that the vortex flap deflection ang...... no benefit in vortex flap deployment at ......to that of the vortex flap. However, when...... used with the vortex flap deflected, these tests showed...

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