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航技研1m×1m超音速風洞のノズル修理後の気流特性
https://jaxa.repo.nii.ac.jp/records/39794
https://jaxa.repo.nii.ac.jp/records/39794b8a3b977-6afc-42e3-9bae-b55fa13555ba
名前 / ファイル | ライセンス | アクション |
---|---|---|
naltm00694.pdf (3.4 MB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 航技研1m×1m超音速風洞のノズル修理後の気流特性 | |||||
言語 | ||||||
言語 | jpn | |||||
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 | AGARD標準模型B | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空力特性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 気流特性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 気流傾斜角 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | マッハ数分布 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 3分力試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ノズル境界層 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 超音速風洞ノズル | |||||
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 | AGARD B standard model | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerodynamic characteristic | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flow characteristic | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flow inclination | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Mach number distribution | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | three component test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | nozzle boundary layer | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | supersonic wind nozzle | |||||
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(英) | ||||||
その他のタイトル | The flow characteristics of the repaired NAL's 1 m x 1 m supersonic wind tunnel | |||||
著者 |
関根, 英夫
× 関根, 英夫× 野田, 順一× 渡辺, 光則× Sekine, Hideo× Noda, Junichi× Watanabe, Mitsunori |
|||||
著者所属 | ||||||
航空宇宙技術研究所 空気力学部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 空気力学部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 空気力学部 | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Aerodynamics Division | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory Aerodynamics Division | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory 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資料 en : Technical Memorandum of National Aerospace Laboratory 巻 694, p. 1-20, 発行日 1996-07 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 航技研の1m×1m超音速風洞のノズルを修理した。修理したノズルは可撓式であり、マッハ数1.4-4.2の範囲で任意のマッハ数に設定可能なものである。この修理工事によってノズル形状を修正すると共に老朽化した部材のオーバーホールを実施した。また、修理前後の測定部流れの傾き角およびマッハ数分布測定ならびにAGARD標準模型Bによる3分力試験を実施し、概ね新設時の特性を持っていることを確認した。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The nozzle of the 1 m x 1 m supersonic wind tunnel of the National Aerospace Laboratory was partially repaired. After the measurement of the nozzle shape dimensions by using a laser measuring instrument, the shape was adjusted to approach to the designed dimensions. The rubber seal was exchanged to a new one. After the repair, the inclination of the flow in the test section was measured using a five hole Pitot tube and the AGARD (Advisory Group for Aerospace Research and Development)-B standard model. Mach number distributions along the nozzle and cross-section of the test section were measured by the static pressures and the Pitot tube. The flow characteristics are close to the one initially designed. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0452-2982 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN00314334 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0000555000 | |||||
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 TM-694 |