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Design and Test of a New Co-axial Air Joints
https://jaxa.repo.nii.ac.jp/records/45173
https://jaxa.repo.nii.ac.jp/records/4517304aff3e2-839c-4cfd-acca-60b30eea8012
名前 / ファイル | ライセンス | アクション |
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naltr00914.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 | Design and Test of a New Co-axial Air Joints | |||||
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 | 偏心ジャーナル空気継手の試作 | |||||
著者 |
野中, 修
× 野中, 修× 中谷, 輝臣× 戸田, 亘洋× 林, 良生× NONAKA, Osamu× NAKAYA, Teruomi× TODA, Nobuhiro× HAYASHI, Yoshio |
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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飛行実験部 | ||||||
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 | ||||||
Flight Research 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-914 巻 914, p. 20, 発行日 1986-09 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In this paper the design and construction of a newly developed co-axial journal air joint is described. This air joint can be used in the wind tunnel testing of a powered model to supply high pressure air for engine simulation without the interference usually caused by stiffness of the air ducts. The air joint is composed of two eccentric floating pieces which are and can be rotated frictionless independently, so that the inner axis may translate within a plane region perpendicular to the axis of rotation. Thus the inner axis can be made to have four degrees of freedom in translation and rotation. Because a large displacement is allowed for the axis, difficulty in setting the model can be greatly reduced. The interference forces were measured with a simulated jet exhaust, and turned out to be negligibly small. | |||||
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: NALTR0914000 | |||||
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-914 |