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二次元風洞におけるAGARD-B標準模型の三分力試験
https://jaxa.repo.nii.ac.jp/records/44222
https://jaxa.repo.nii.ac.jp/records/44222ef8f0ea4-7ce3-47e2-a0ba-92ad9e8aa735
名前 / ファイル | ライセンス | アクション |
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naltm00639.pdf (1.3 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 | ||||||
タイトル | 二次元風洞におけるAGARD-B標準模型の三分力試験 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | transonic flow; two-dimensional wind tunnel; force measurement tests | |||||
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 | Force Measurements on AGARD Calibration Model-B at Transonic Speeds in the NAL Two-Dimensional Wind Tunnel | |||||
著者 |
佐藤, 衛
× 佐藤, 衛× 神田, 宏× 須谷, 記和× 馬場, 滋夫× 三輪, 等× 河本, 巌× SATO, Mamoru× KANDA, Hiroshi× SUDANI, Norikazu× BABA, Shigeo× MIWA, Hitoshi× KAWAMOTO, Iwao |
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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 | ||||||
航空宇宙技術研究所空力性能部 | ||||||
著者所属(英) | ||||||
en | ||||||
Aircraft Aerodynamics Division | ||||||
著者所属(英) | ||||||
en | ||||||
Aircraft Aerodynamics Division | ||||||
著者所属(英) | ||||||
en | ||||||
Aircraft Aerodynamics Division | ||||||
著者所属(英) | ||||||
en | ||||||
Aircraft Aerodynamics Division | ||||||
著者所属(英) | ||||||
en | ||||||
Aircraft Aerodynamics Division | ||||||
著者所属(英) | ||||||
en | ||||||
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資料 en : Technical Memorandum of National Aerospace Laboratory 巻 639, p. 12, 発行日 1991-08 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In order to investigate the capability of conducting force measurements of three-dimensional (3-D) models in NAL′s two-dimensional (2-D) wind tunnel, force measurements on AGARD calibration Model-B (Mach numbers: 0.5-1.1, Reynolds number : 3×106and 4×106). Full and half models were tested. Four different strut lengths having a circular arc cross-section and stings were used to install the full model. For the half model, a plate was installed to remove the effects of the wind tunnel′s sidewall boundary layer, as well as adding a small gap between the model and the plate to remove the effects of the plate′s boundary layer. It was shown that force measurements of 3-D models are possible in NAL′s 2-D wind tunnel, although improvements in the struts and stings are necessary to conduct tests at Mach numbers greater than 0.85. | |||||
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: NALTM0639000 | |||||
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-639 |