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Construction and Performance of NAL Two-Dimensional Transonic Wind Tunnel
https://jaxa.repo.nii.ac.jp/records/44903
https://jaxa.repo.nii.ac.jp/records/4490357a434f9-ec2e-4339-98b2-21f83a298cfe
| 名前 / ファイル | ライセンス | アクション |
|---|---|---|
naltr0647t.pdf (5.6 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 | Construction and Performance of NAL Two-Dimensional Transonic Wind Tunnel | |||||||||
| 言語 | en | |||||||||
| 言語 | ||||||||||
| 言語 | eng | |||||||||
| 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 | |||||||||
| 著者 |
空気力学第二部
× 空気力学第二部
× Second, Aerodynamics Division
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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（英） | ||||||||||
| en | ||||||||||
| Second Aerodynamics Division, National Aerospace Laboratory(NAL) | ||||||||||
| 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 |
en : Technical Report of National Aerospace Laboratory TR-647T 巻 647T, p. 50, 発行日 1982-02 |
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| 抄録（英） | ||||||||||
| 内容記述タイプ | Other | |||||||||
| 内容記述 | The construction and the results of initial calibration are described in this report. This tunnel was built to meet the requirements of high Reynolds number testing of wing sections at transonic regime. It is a blowdown tunnel with a test section of 0.3m×1.0m. The required capability of this wind tunnel is for Mach numbers ranging from 0.2 to 1.2 and for a Reynolds number up to 40×10(exp 6) at Mach number 0.8 with sufficient running time. First, an outline of the design objectives is given. Secondly, the completed facilities, i.e., the wind tunnel, the instrumentation and operation system, the silencer and auxiliary equipment of the air compressor and the air reservoir, are described in detail. Finally, the performance of the tunnel is described based on experimental results. High Reynolds number testing can be achieved in this wind tunnel without any trouble. Reynolds number effects on the airfoil characteristics are clarified experimentally. | |||||||||
| 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: NALTR0647T000 | |||||||||
| 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-647T | |||||||||
