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Preliminary study of a model rotor in descent [microform] / K.W. McAlister ... [et al.] ([NASA technical memorandum] ; NASA/TM-2000-208785)

Preliminary study of a model rotor in descent [microform] / K.W. McAlister ... [et al.] ([NASA technical memorandum] ; NASA/TM-2000-208785)
Microform図書
2000<YCA-NAS 1.15:208785>
National Diet Library
  • Subject HeadingTrajectories Vortices Blade-vortex interaction Helicopter tail rotors Helico...

Full-potential modeling of blade-vortex interactions [microform] / Henry E. Jones (NASA technical paper ; 3651)

Full-potential modeling of blade-vortex interactions [microform] / Henry E. Jones (NASA technical paper ; 3651)
Microform図書
1997<YCA-NAS 1.60:3651>
National Diet Library
  • Subject HeadingBlade-vortex interaction Unsteady flow Transonic flow ...

Helicopter blade-vortex interaction noise with comparisons to CFD calculations [microform] / Megan S. McCluer (NASA technical memorandum ; 110423)

Helicopter blade-vortex interaction noise with comparisons to CFD calculations [microform] / Megan S. McCluer (NASA technical memorandum ; 110423)
Microform図書
1996<YCA-NAS 1.15:110423>
National Diet Library
  • Subject HeadingBlade-vortex interaction Blade slap noise Computationa...

Predicted aerodynamic characteristics of a NACA 0015 airfoil having a 25% integral-type trailing edge flap [microform] / Ahmed Hassan ([NASA contractor report] ; NASA/CR-1999-209328)

Predicted aerodynamic characteristics of a NACA 0015 airfoil having a 25% integral-type trailing edge flap [microform] / Ahmed Hassan ([NASA contractor report] ; NASA/CR-1999-209328)
Microform図書
1999<YCA-NAS 1.26:209328>
National Diet Library
  • Subject HeadingNoise reduction Airfoils Blade-vortex interaction Navier-Stokes equation Traili...

Reduction of helicopter blade-vortex interaction noise by active rotor control technology [microform] / Yung H. Yu ... [et al.] (NASA/TM ; 207568)

Reduction of helicopter blade-vortex interaction noise by active rotor control technology [microform] / Yung H. Yu ... [et al.] (NASA/TM ; 207568)
Microform図書
1997<YCA-NAS 1.15:207568>
National Diet Library
  • Subject HeadingActive control Blade-vortex interaction Control systems design Smart ...

Helicopter rotor blade computation in unsteady flows using moving overset grids [microform] / Jasim Ahmad and Earl P.N. Duque ([NASA technical memorandum] ; 207307)

Helicopter rotor blade computation in unsteady flows using moving overset grids [microform] / Jasim Ahmad and Earl P.N. Duque ([NASA technical memorandum] ; 207307)
Microform図書
1996<YCA-NAS 1.15:207307>
National Diet Library
  • Subject HeadingBlade-vortex interaction Rotary wing aircraft Computat...

New computational methods for the prediction and analysis of helicopter noise [microform] / Roger C. Strawn, Leonid Oliker, Rupak Biswas ([NASA contractor report] ; NASA-CR-201384) (RIACS technical report ; 96.10)

New computational methods for the prediction and analysis of helicopter noise [microform] / Roger C. Strawn, Leonid Oliker, Rupak Biswas ([NASA contractor report] ; NASA-CR-201384) (RIACS technical report ; 96.10)
Microform図書
1996<YCA-NAS 1.26:201384>
National Diet Library
  • Subject Heading...ics Far fields Blade-vortex interaction Noise propagation Noise predi...

Reynolds-averaged Navier-Stokes studies of low Reynolds number effects on the losses in a low pressure turbine [microform] / Daniel J. Dorney (NASA contractor report ; 198534)

Reynolds-averaged Navier-Stokes studies of low Reynolds number effects on the losses in a low pressure turbine [microform] / Daniel J. Dorney (NASA contractor report ; 198534)
Microform図書
1996<YCA-NAS 1.26:198534>
National Diet Library
  • Subject Heading...y aerodynamics Blade-vortex interaction Rotor stator interactions Pro...

Blade-mounted flap control for BVI noise reduction proof-of-concept test [microform] / Seth Dawson ... [et al] (NASA contractor report ; 195078)

Blade-mounted flap control for BVI noise reduction proof-of-concept test [microform] / Seth Dawson ... [et al] (NASA contractor report ; 195078)
Microform図書
1995<YCA-NAS 1.26:195078>
National Diet Library
  • Subject HeadingBlade-vortex interaction Wind tunnel tests Noise reduc...

A parametric study on parallel blade-vortex interaction for helicopter rotor

A parametric study on parallel blade-vortex interaction for helicopter rotor
Digital文書・図像類
田辺, 安忠, 齊藤, 茂, 高崎, 啓介, 藤田, 肇, Tanabe, Yasutada, Saito, Shigeru, Takasaki, Keisuke, Fujita, Hajime宇宙航空研究開発機構2008-02-29宇宙航空研究開発機構研究開発報告 = JAXA Research and Development ReportJAXA-RR-07-051E
Other Libraries in Japan
  • Subject Heading... 翼型 helicopter blade-vortex interaction miss distance rotary wing par...
  • Note (General)並行ブレード／渦干渉(BVI: Blade-Vortex Interaction)についてパラメトリック研究を......dy on parallel Blade-Vortex Interaction (BVI) is carried out. A high ...

Inviscid numerical simulations of 2D parallel blade-vortex interaction JAXA/ONERA cooperation

Inviscid numerical simulations of 2D parallel blade-vortex interaction JAXA/ONERA cooperation
Digital文書・図像類
田辺, 安忠, 齊藤, 茂, Yang, Choongmo, 青山, 剛史, Benoit, C., Gretay, J. O., Jeanfaivre, G., Peron, S., Sides, J., Tanabe, Yasutada, Saito, Shigeru, Aoyama, Takashi宇宙航空研究開発機構2007-03-30宇宙航空研究開発機構研究開発報告 = JAXA Research and Development ReportJAXA-RR-06-042E
Other Libraries in Japan
  • Subject Heading...cal simulation blade-vortex interaction helicopter aerodynamic noise ...
  • Note (General)... Dynamics)とBVI(Blade-Vortex Interaction)騒音予測方法の比較研究」のタ......ional parallel blade-vortex interaction are carried ou......mics) and BVI (Blade-Vortex Interaction) noise predict......es of parallel Blade-Vortex Interaction is evaluated. The results fro...

Numerical study on the lateral jet flow of helicopter rotor

Numerical study on the lateral jet flow of helicopter rotor
Digital文書・図像類
Yang, Choongmo, 青山, 剛史, 齊藤, 茂, Baek, Jehyun, Aoyama, Takashi, Saito, Shigeru宇宙航空研究開発機構2005-01-31宇宙航空研究開発機構研究開発報告 = JAXA Research and Development ReportJAXA-RR-04-014E
Other Libraries in Japan
  • Subject Heading...ズム ベクトル演算 騒音予測 blade-vortex interaction Euler equation of motion heli...
  • Note (General)ブレード／渦干渉(Blade-Vortex Interaction: BVI)騒音は、先行するメイン・ロータのブレードが吐き出...

1枚ブレード・モデル・ロータを使ったアクティブ・ブレード・コントロール風洞試験

1枚ブレード・モデル・ロータを使ったアクティブ・ブレード・コントロール風洞試験
Digital文書・図像類
近藤, 夏樹, 末永, 尚史, 白井, 正孝, 齊藤, 茂, 赤坂, 剛史, 田辺, 安忠, Kondo, Natsuki, Suenaga, Hisashi, Shirai, Masataka, Saito, Shigeru, Akasaka, Takeshi, Tanabe, Yasutada航空宇宙技術研究所2003-05航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory771
Other Libraries in Japan
  • Subject Heading...rmonic control blade-vortex interaction vortex generator amplitude ph...
  • Note (General)...緩降下飛行中に発生するBVI(Blade-Vortex Interaction:ブレード／渦干渉)騒音に対し......(AFC) on rotor blade-vortex interaction (BVI) noise were investigated...

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