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高速軸流圧縮機の研究[Ⅳ]-NACA65系翼型を修正した近似二重円弧翼形の動翼相対入口マッハ数1.5までの回転翼列試験-
https://jaxa.repo.nii.ac.jp/records/44317
https://jaxa.repo.nii.ac.jp/records/44317aae68409-21f1-4247-b010-d9f219eac131
名前 / ファイル | ライセンス | アクション |
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naltr00076.pdf (1.8 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 | 高速軸流圧縮機の研究[Ⅳ]-NACA65系翼型を修正した近似二重円弧翼形の動翼相対入口マッハ数1.5までの回転翼列試験- | |||||
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 | An Investigation of High Speed Axial Flow Compressor[IV]-Rotor Performance at Relative Inlet Mach Numbers up to 1.5 of NACA 65-Series Compressor Blades Modified Approximately to Double Circular-Arc Blades- | |||||
著者 |
大山, 耕一
× 大山, 耕一× 松木, 正勝× 西脇, 英夫× 岩部, 柱相× 片山, 康治× OYAMA, Koichi× MATSUKI, Masakatsu× NISHIWAKI, Hideo× IWABE, Tadasuke× KATAYAMA, Yasuharu |
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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(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 en : Technical Report of National Aerospace Laboratory TR-76 巻 76, p. 33, 発行日 1965-01 |
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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: NALTR0076000 | |||||
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-76 |