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高速軸流圧縮機の研究〔Ⅲ〕-翼の厚さの影響-
https://jaxa.repo.nii.ac.jp/records/44287
https://jaxa.repo.nii.ac.jp/records/44287d451811e-4a17-41be-9b5e-eabf803422e2
名前 / ファイル | ライセンス | アクション |
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naltr00049.pdf (893.3 kB)
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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 | 高速軸流圧縮機の研究〔Ⅲ〕-翼の厚さの影響- | |||||
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 | An Investigation of High Speed Axial Flow Compressor〔III〕 Effects of Blade Thickness | |||||
著者 |
松木, 正勝
× 松木, 正勝× 宮地, 敏雄× 大山, 耕一× 吉田, 晃× 西脇, 英夫× 岩部, 柱相× MATSUKI, Masakatsu× MIYACHI, Toshio× OYAMA, Koichi× YOSHIDA, Akira× NISHIWAKI, Hideo× IWABE, Tadasuke |
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著者所属 | ||||||
航空宇宙技術研究所原動機部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所原動機部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所原動機部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所原動機部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所原動機部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所原動機部 | ||||||
著者所属(英) | ||||||
en | ||||||
Aeroengine Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Aeroengine Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Aeroengine Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Aeroengine Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Aeroengine Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Aeroengine 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TR-49 en : TECHNICAL REPORT OF NATIONAL AERONAUTICAL LABORATORY TR-49 巻 49, p. 13, 発行日 1963-09 |
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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: NALTR0049000 | |||||
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-49 |