WEKO3
アイテム
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航技研0.1m×0.1m遷音速低温風洞の気流測定
https://jaxa.repo.nii.ac.jp/records/41206
https://jaxa.repo.nii.ac.jp/records/41206ec03a354-880f-4118-a895-7e1d0aa6c72d
名前 / ファイル | ライセンス | アクション |
---|---|---|
naltr01221.pdf (1.5 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0.1m×0.1m遷音速低温風洞の気流測定 | |||||
言語 | ||||||
言語 | jpn | |||||
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 | 低温環境試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 流れ計測 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 流れトラバース装置 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 精密位置設定 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風洞気流特性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 高レイノルズ数風洞 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ヨーメータ特性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 遠隔操作システム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 測定部 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 総圧分布 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風向分布 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ピトー管振動 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 器差 | |||||
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 | cryogenic environment test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flow measurement | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flow traversing device | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | precision position setting | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind tunnel flow quality | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | high Reynolds number wind tunnel | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | yaw meter characteristic | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | remote control system | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | test section | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | total pressure distribution | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind direction distribution | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | pitot tube vibration | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | instrument bias error | |||||
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 | Measurement of free-stream properties in the NAL 0.1 m X 0.1 m transonic cryogenic wind tunnel | |||||
著者 |
青木, 竹夫
× 青木, 竹夫× 澤田, 秀夫× Aoki, Takeo× Sawada, Hideo |
|||||
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 | ||||||
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 1221, p. 1-13, 発行日 1993-12 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 航空宇宙技術研究所(NAL)0.1m×0.1m遷音速低温風洞における気流の性質を、低温風洞用に特に設計したトラバース装置を用いて測定した。このトラバース装置は、93Kの低温で作動するステイングースラットシステム、ステップモータ、ギアボックス、およびボールベアリングよりなる。総温プローブ、ピトー管、静圧管、ヨーメータ(2次元)のような種々のプローブをこの装置に取り付けることができる。気流測定の結果の概要は次のとおりである。測定部断面における総温と総圧変動はそれぞれ1.5Kおよび0.1%以内であった。静圧分布のデータは、風洞の中心線回りの流速は上部および下部近くの壁のそれより0.1-0.2%大きいことを示す。風向の測定は、試験断面ではマッハ数0.8において流れが拡がることを示す。流れの方向の最大の差は0.62度ある。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Free-stream properties in the NAL 0.1 m X 0.1 m Transonic Cryogenic Wind Tunnel were measured by using a traversing device especially designed for use in cryogenic wind tunnels. This traversing device consists of a sting-strut system, a stepping motor, a gear box, and ball bearings which can operate under cryogenic environments as cold as 93 K. Various probes such as a total temperature probe, a pitot tube, a static probe, and a yawmeter (two dimensional) can be mounted on this device. The results of free-stream measurements can be summarized as follows: Variations of total temperature and total pressure in the test section were within 1.5 K and 0.1 percent, respectively; The static pressure distribution data indicate that flow velocity around the tunnel center line is 0.1 - 0.2 percent greater than that near the upper and lower walls. Measurement of flow angularity shows that the flow diverges in the test section at Mach number 0.8. The maximum difference in the flow direction is 0.62 deg. | |||||
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: AA0004236000 | |||||
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-1221 |