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検索結果 8 件

A parametric study of accelerations of an airplane due to a wake vortex system [microform] / Eric C. Stewart ([NASA technical memorandum] ; NASA/TM-1999-208745)

A parametric study of accelerations of an airplane due to a wake vortex system [microform] / Eric C. Stewart ([NASA technical memorandum] ; NASA/TM-1999-208745)
マイクロ図書
1999<YCA-NAS 1.15:208745>
国立国会図書館
  • 件名...w distribution Rectangular wings Roll Rotation Vortices Yaw A...

Computational test cases for a rectangular supercritical wing undergoing pitching oscillations [microform] / Robert M. Bennett and Charlotte E. Walker ([NASA technical memorandum] ; NASA/TM-1999-209130)

Computational test cases for a rectangular supercritical wing undergoing pitching oscillations [microform] / Robert M. Bennett and Charlotte E. Walker ([NASA technical memorandum] ; NASA/TM-1999-209130)
マイクロ図書
1999<YCA-NAS 1.15:209130>
国立国会図書館
  • 件名...y aerodynamics Rectangular wings Supercritical wings Wing osc...

Cellular structures in the flow over the flap of a two-element wing [microform] / Steven A. Yon and Joseph Katz ([NASA contractor report] ; 112613)

Cellular structures in the flow over the flap of a two-element wing [microform] / Steven A. Yon and Joseph Katz ([NASA contractor report] ; 112613)
マイクロ図書
1997<YCA-NAS 1.26:112613>
国立国会図書館
  • 件名...ime dependence Rectangular wings Angle of attack Pressure rat...

The AFDD International Dynamic Stall Workshop on correlation of dynamic stall models with 3-D dynamic stall data [microform] / C.M. Tan and L.W. Carr (NASA technical memorandum ; 110375)

The AFDD International Dynamic Stall Workshop on correlation of dynamic stall models with 3-D dynamic stall data [microform] / C.M. Tan and L.W. Carr (NASA technical memorandum ; 110375)
マイクロ図書
1996<YCA-NAS 1.15:110375>
国立国会図書館
  • 件名...cillating flow Rectangular wings Unswept wings Wing oscillati...

Study of the unsteady flow features on a stalled wing [microform] / S. Yon and J. Katz ([NASA contractor report] ; 112612)

Study of the unsteady flow features on a stalled wing [microform] / S. Yon and J. Katz ([NASA contractor report] ; 112612)
マイクロ図書
1997<YCA-NAS 1.26:112612>
国立国会図書館
  • 件名...c wind tunnels Rectangular wings Flow distribution Separated ...

Measurements of supersonic wing tip vortices [microform] : 18th AIAA Aerospace Ground Testing Conference, June 20-23, 1994/Colorado Springs, CO / M.K. Smart, I.M. Kalkhoran and J. Bentson ([NASA contractor report] ; NASA-CR-202591)

Measurements of supersonic wing tip vortices [microform] : 18th AIAA Aerospace Ground Testing Conference, June 20-23, 1994/Colorado Springs, CO / M.K. Smart, I.M. Kalkhoran and J. Bentson ([NASA contractor report] ; NASA-CR-202591)
マイクロ図書
1994<YCA-NAS 1.26:202591>
国立国会図書館
  • 件名...re measurement Rectangular wings Supersonic speed

Application of the wake integral method to CFD data

Application of the wake integral method to CFD data
デジタル文書・図像類
上野, 真, 赤塚, 純一, Ueno, Makoto, Akatsuka, Junichi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-07-030E
全国の図書館
  • 件名... configuration rectangular wing

低レイノルズ数における翼の2次元非定常空力特性の実験的研究

低レイノルズ数における翼の2次元非定常空力特性の実験的研究
デジタル文書・図像類
岡本, 正人, 藤枝, 郭俊, 東, 昭, Okamoto, Masato, Fujieda, Hirotoshi, Azuma, Akira航空宇宙技術研究所2002-11航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1453
全国の図書館
  • 件名...ow insect bird rectangular wing aspect ratio research and dev...
  • 一般注記...tent possible. Rectangular wings, with various sections made ...

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