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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)
Microform図書
1999<YCA-NAS 1.15:208745>
National Diet Library
  • Subject Heading...w distribution Rectangular wings Roll Rotation Vortices Yaw Ai...

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)
Microform図書
1999<YCA-NAS 1.15:209130>
National Diet Library
  • Subject Heading...y aerodynamics Rectangular wings Supercritical wings Wing osci...

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)
Microform図書
1997<YCA-NAS 1.26:112613>
National Diet Library
  • Subject Heading...ime dependence Rectangular wings Angle of attack Pressure rati...

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)
Microform図書
1996<YCA-NAS 1.15:110375>
National Diet Library
  • Subject Heading...cillating flow Rectangular wings Unswept wings Wing oscillatio...

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)
Microform図書
1997<YCA-NAS 1.26:112612>
National Diet Library
  • Subject Heading...c wind tunnels Rectangular wings Flow distribution Separated f...

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)
Microform図書
1994<YCA-NAS 1.26:202591>
National Diet Library
  • Subject Heading...re measurement Rectangular wings Supersonic speed

Application of the wake integral method to CFD data

Application of the wake integral method to CFD data
Digital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
Other Libraries in Japan

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
Digital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
Other Libraries in Japan
  • Note (General)...tent possible. Rectangular wings, with various sections made o...

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