Výsledky vyhledávání - "境界層厚さ"

Publikováno v: 宇宙航空研究開発機構特別資料: 境界層遷移の解明と制御研究会講演論文集第39回 = JAXA Special Publication: Proceedings of the 39th JAXA Workshops on Investigation and Control of Boundary-Layer Transition. :23-26

This numerical study examines the supersonic rectangular-nozzle flow by focusing attention on the development of secondary flow and corner-flow and their effects on the boundary layer instability and transition. The results show that secondary flows

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::a8e39b3a33af7fd90a3787c816692c14
http://id.nii.ac.jp/1696/00005647/

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Preliminary report of the blockage data in JAXA 1 m x 1 m Supersonic Wind Tunnel

Autor: Iijima, Hidetoshi, Sato, Mamoru, Watanabe, Mitsunori, Nagai, Shinji, Itabashi, Yukihiro, Nishijima, Hironori, Kimura, Takeshi

Publikováno v: 宇宙航空研究開発機構特別資料: 第76回風洞研究会議論文集 = JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 76th Meeting. :33-37

JAXA1m×1m超音速風洞における風洞始動限界を、異なるブロッケージ比の円盤および正方形板模型を用いて調べた。また、その妥当性を確認するために、他風洞の結果と比較した。さらに、

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http://id.nii.ac.jp/1696/00005836/

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境界層遷移に対する主流乱れのスケールの影響

Autor: Kenchi, Toshiaki, Matsubara, Masaharu

Publikováno v: 宇宙航空研究開発機構特別資料: 境界層遷移の解明と制御研究会講演論文集第35回・第36回 = JAXA Special Publication: Proceedings of the 35th and 36th JAXA Workshops on Investigation and Control of Boundary-Layer Transition. :11-14

The present experiment focused on revealing effect of scales and directional components of free stream turbulence on boundary layer transition, especially the growth rate of the disturbance energy in the streamwise direction. Free stream turbulence g

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::5eb4ecc5886170b4fc074a63d3224eec
http://id.nii.ac.jp/1696/00006180/

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A measurement of turbulent boundary layer thickness at the JAXA 1 m x 1 m supersonic wind tunnel

Autor: Watanabe, Mitsunori, Iijima, Hidetoshi, Sato, Mamoru, Nagai, Shinji, Nishijima, Hironori, Kimura, Tsuyoshi, Itabashi, Yukihiro

Publikováno v: 宇宙航空研究開発機構特別資料: 第72回風洞研究会議論文集 = JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 72nd Meeting. :6-13

JAXA吹出式1m×1m超音速風洞においては、1999年度から2000年度に行われた風洞改修後ユーザ試験と並行して、各種の気流特性試験を実施している。本報告では、風洞測定部中心下壁において�

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http://id.nii.ac.jp/1696/00006430/

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乱流境界層の構造と渦

Autor: Kobashi, Yasujiro, Hayakawa, Michio

Publikováno v: 宇宙航空研究開発機構特別資料: 境界層遷移の解明と制御研究会講演論文集第33回・第34回 = JAXA Special Publication: Proceedings of the 33rd and 34th JAXA Workshops on Investigation and Control of Boundary-Layer Transition. :5-8

Based on the idea that turbulence is the flow phenomena caused by the movement of vortex, the structures of turbulent boundary layer are discussed. The circulation is the most important factor for characterizing the flow structures. The large scale m

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http://id.nii.ac.jp/1696/00006550/

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Design and control of crossflow instability field

Autor: Kohama, Yasuaki, Onodera, Tatsuya

Publikováno v: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory. 28:3-6

航空宇宙技術研究所 Sep. 1994 (15th). Mar. 1995 (16th) 東京日本
National Aerospace Laboratory Sep. 1994 (15th). Mar. 1995 (16th) Tokyo Japan
横流れの支配的な境界層を制御するために、排除体を伴った偏�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::fbfedb24b90405530b6a35b9b63f5d85
http://id.nii.ac.jp/1696/00036724/

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Proceedings of the Wind Tunnel Technology Association 76th Meeting

Autor: Japan Aerospace Exploration Agency

Publikováno v: 宇宙航空研究開発機構特別資料 = JAXA Special Publication.

20060525-20060526
資料番号: AA0063330000
レポート番号: JAXA-SP-06-020

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::075a08bb6b7a24331eb3beb5b3bed76b
http://id.nii.ac.jp/1696/00005829/

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