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高速翼列の実験について(流入角の大きい減速翼列の予備実験)
https://jaxa.repo.nii.ac.jp/records/44282
https://jaxa.repo.nii.ac.jp/records/442825892b13b-c479-4a95-8e30-9ebc77cc35c3
名前 / ファイル | ライセンス | アクション |
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naltr00044.pdf (7.0 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 | 高速翼列の実験について(流入角の大きい減速翼列の予備実験) | |||||
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 | Some Notes about the Effect of Tunnel Configuration and Testing Technique on Compressor Cascade Performance | |||||
著者 |
近藤, 博
× 近藤, 博× 蓑田, 光弘× 坂口, 一× 山崎, 紀雄× KONDO, Hiroshi× MINODA, Mitsuhiro× SAKAGUCHI, Hajime× YAMAZAKI, Norio |
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著者所属 | ||||||
航空技術研究所原動機部 | ||||||
著者所属 | ||||||
航空技術研究所原動機部 | ||||||
著者所属 | ||||||
航空技術研究所原動機部 | ||||||
著者所属 | ||||||
航空技術研究所原動機部 | ||||||
著者所属(英) | ||||||
en | ||||||
Aeroengine Division, National Aeronautical Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Aeroengine Division, National Aeronautical Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Aeroengine Division, National Aeronautical Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Aeroengine Division, National Aeronautical Laboratory(NAL) | ||||||
出版者 | ||||||
出版者 | 航空技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aeronautics Laboratory(NAL) | |||||
書誌情報 |
航空技術研究所報告TR-44 en : TECHNICAL REPORT OF NATIONAL AERONAUTICAL LABORATORY TR-44 巻 44, p. 30, 発行日 1963-02 |
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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: NALTR0044000 | |||||
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-44 |