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二次元風胴構成要素の研究(Ⅳ)-消音装置の設計と性能試験-
https://jaxa.repo.nii.ac.jp/records/44861
https://jaxa.repo.nii.ac.jp/records/4486175dc33bf-e348-463b-9945-6cb6882febd0
名前 / ファイル | ライセンス | アクション |
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naltr00606.pdf (2.8 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 | 二次元風胴構成要素の研究(Ⅳ)-消音装置の設計と性能試験- | |||||
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 | Investigation of the Components of the NAL High Reynolds Number Two-Dimensional Wind Tunnel, Part IV Design, Construction and Performance of the Exhaust Silencer | |||||
著者 |
榊原, 盛三
× 榊原, 盛三× 三輪, 等× 萱場, 重男× 佐藤, 衛× SAKAKIBARA, Seizo× MIWA, Hitoshi× KAYABA, Shigeo× SATO, Mamoru |
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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 | ||||||
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) | ||||||
著者所属(英) | ||||||
en | ||||||
Second Aerodynamics Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Second Aerodynamics Division, National Aerospace Laboratory(NAL) | ||||||
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 |
航空宇宙技術研究所報告 en : Technical Report of National Aerospace Laboratory TR-606 巻 606, p. 17, 発行日 1980-04 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | This paper presents a description of the design, construction and performance of the exhaust silencer for the NAL high Reynolds number two-dimensional transonic blow down wind tunnel, which was completed in October 1979. The silencer is a twostoried construction made of reinforced concrete, 40M long, 10M wide and 19M high, and entirely enclosed by thick concrete walls. The upstream part of the first story, particularly, is covered with double walls, the thickness of the two walls being 0.3M(inner wall) and 0.2M(outer wall), respectively. A noise reduction system using three kinds of parallel baffles and two kinds of lined bends is adopted for the wind tunnel exhaust noise. | |||||
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: NALTR0606000 | |||||
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-606 |