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The NAL 0.2 m supersonic wind tunnel
https://jaxa.repo.nii.ac.jp/records/39808
https://jaxa.repo.nii.ac.jp/records/39808e772a0b5-1c50-4042-97e6-daab503a98a7
名前 / ファイル | ライセンス | アクション |
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naltr1302t.pdf (1.9 MB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | The NAL 0.2 m supersonic wind tunnel | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 超音速風洞 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軸流圧縮機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 高研磨縮流面 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 低温風洞 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 縮流比 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 低乱化 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 高レイノルズ数 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 可変マッハ数ノズル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 境界層吸い取り装置 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | supersonic wind tunnel | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | axial flow compressor | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | highly polished contraction surface | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | cryogenic wind tunnel | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | contraction ratio | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | turbulence reduction | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | high Reynolds number | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | variable Mach number nozzle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | boundary layer suction device | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル | ||||||
その他のタイトル | NAL0.2m超音速風洞 | |||||
著者 |
澤田, 秀夫
× 澤田, 秀夫× 鈴木, 弘一× 半沢, 麻雄× 河野, 敬× 国益, 徹也× Sawada, Hideo× Suzuki, Koichi× Hanzawa, Asao× Kono, Takashi× Kunimasu, Tetsuya |
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著者所属 | ||||||
航空宇宙技術研究所 空力性能部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 空力性能部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 空力性能部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 空力性能部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 空力性能部 | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Aircraft Aerodynamics Division | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Aircraft Aerodynamics Division | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Aircraft Aerodynamics Division | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Aircraft Aerodynamics Division | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Aircraft Aerodynamics Division | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory (NAL) | |||||
書誌情報 |
航空宇宙技術研究所報告 en : Technical Report of National Aerospace Laboratory 巻 1302T, p. 1-10, 発行日 1996-07 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 1995年に小型超音速風洞(航技研0.2m超音速風洞)が航空宇宙技術研究所に新たに作られた。測定部は断面が0.2m×0.2mで長さが0.4mである。マッハ数は可変ノズルにより1.5から2.5までの任意の値に設定できる。総圧は0.15MPaまでで、総温は約330Kである。本風洞は主構造材と圧縮機が低温で使えるように設計されていることと、測定部面積に対する縮流比は約28もあり、境界層吸い取り装置が縮流部に設け、流れの低乱化を図っていることの2つの特徴を持つ。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A small supersonic wind tunnel (The NAL 0.2 m supersonic wind tunnel) was built at the National Aerospace Laboratory, Japan in 1995. The test section is 0.2 m x 0.2 m in cross section and 0.4 m long. Mach number can be set to any value from 1.5 to 2.5 by its flexible plate nozzle. Total pressure can be up to 0.15 MPa and total temperature is around 330 K. This tunnel has two unique points. The main structure and compressor were designed to be available at cryogenic temperatures. The contraction ratio to the test section is about 28, and the boundary layer suction device is mounted at the contraction, in order to establish low turbulent flow. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0389-4010 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0000596000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL TR-1302T |