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Investigation of ATP blades(PartI): Test of Thin Airfoils in the NAL 2-D Transonic Wind Tunnel
https://jaxa.repo.nii.ac.jp/records/44198
https://jaxa.repo.nii.ac.jp/records/44198275bac17-4568-440d-8711-c055ed0adab0
名前 / ファイル | ライセンス | アクション |
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naltm00615.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 | ||||||
言語 | en | |||||
タイトル | Investigation of ATP blades(PartI): Test of Thin Airfoils in the NAL 2-D Transonic Wind Tunnel | |||||
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 | |||||
その他のタイトル | ||||||
その他のタイトル | ATPブレードの研究(I): 薄翼の遷音速二次元風洞試験 | |||||
著者 |
佐藤, 衛
× 佐藤, 衛× 神田, 宏× 須谷, 記和× 小国, 保男× 馬場, 滋夫× 三輪, 等× 河本, 巌× 少路, 宏和× 大竹, 邦彦× 菊野, 栄次× 市川, 恵通× 遠藤, 宏× 信谷, 英之× SATO, Mamoru× KANDA, Hiroshi× SUDANI, Norikazu× OGUNI, Yasuo× BABA, Shigeo× MIWA, Hitoshi× KAWAMOTO, Iwao× SHOJI, Hirokazu× OOTAKE, Kunihiko× KIKUNO, Eiji× ICHIKAWA, Yoshimichi× ENDO, Hiroshi× NOBUTANI, Hideyuki |
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著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
住友精密工業株式会社 | ||||||
著者所属 | ||||||
住友精密工業株式会社 | ||||||
著者所属 | ||||||
住友精密工業株式会社 | ||||||
著者所属 | ||||||
住友精密工業株式会社 | ||||||
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資料 en : Technical Memorandum of National Aerospace Laboratory 巻 615, p. 48, 発行日 1989-11 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Two-dimensional transonic wind tunnel tests of thin airfoils were made as a part of aerodynamic research on propeller blades for advanced turboprop engines. The test airfoils were NACA-16-202 and NACA16-204 which were developed as airfoils for conventional propeller systems at NACA in 1934. The Reynolds number is 8×106. The Mach number was varied from 0.6 to 1.0 and angles of attack from -10 to +16. In addition, vibration characteristics were measured and analyzed. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0452-2982 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN00314334 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: NALTM0615000 | |||||
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 TM-615 |