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Bibliographic Record
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- Material Type
- 規格・テクニカルリポート類
- Title
- Author/Editor
- 高島, 一明沢田, 秀夫青木, 竹夫TAKASHIMA, KazuakiSAWADA, HideoAOKI, Takeo
- Publication, Distribution, etc.
- Publication Date
- 1981-08
- Publication Date (W3CDTF)
- 1981-08
- Alternative Title
- A Survey of the Three-Dimensional High Reynolds Number Transonic Wind Tunnel
- Periodical title
- 航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory
- No. or year of volume/issue
- 440
- Volume
- 440
- Pages
- 38-
- ISSN (Periodical Title)
- ISSN : 0452-2982
- Text Language Code
- jpn
- Target Audience
- 一般
- Note (General)
- 出版タイプ： NAA 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.資料番号: NALTM0440000レポート番号: NAL TM-440
- Periodical Title (NCID)
- AN00314334
- Data Provider (Database)
- 国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
- Original Data Provider (Database)
- 宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ