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三次元レイノルズ数遷音速風胴の調査研究
https://jaxa.repo.nii.ac.jp/records/44023
https://jaxa.repo.nii.ac.jp/records/44023b31a3585-4968-40bd-aa69-9235ed975195
名前 / ファイル | ライセンス | アクション |
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naltm00440.pdf (3.0 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 | 三次元レイノルズ数遷音速風胴の調査研究 | |||||
言語 | ||||||
言語 | jpn | |||||
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 | A Survey of the Three-Dimensional High Reynolds Number Transonic Wind Tunnel | |||||
著者 |
高島, 一明
× 高島, 一明× 沢田, 秀夫× 青木, 竹夫× TAKASHIMA, Kazuaki× SAWADA, Hideo× AOKI, Takeo |
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著者所属 | ||||||
航空宇宙技術研究所空気力学第二部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所空気力学第二部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所空気力学第二部 | ||||||
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 440, p. 38, 発行日 1981-08 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A survey of the facilities for aerodynamic testing of airplane models at transonic speeds and high Reynolds numbers is presented.At first,the need for high Reynolds number transonic testing is reviewed,using some experimental results.Then,some new approaches to high Reynolds number testing,i.e.the cryogenic wind tunnel,the induction driven wind tunnel,the Ludwieg tube,the Evans clean tunnel and the hydraulic driven wind tunnel are described.Finally,this paper comments upon the level of development of high Reynolds number testing facilities in this country. | |||||
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: NALTM0440000 | |||||
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-440 |