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気流全温度測定装置の試作
https://jaxa.repo.nii.ac.jp/records/44503
https://jaxa.repo.nii.ac.jp/records/44503f98abacb-0024-4e81-a30e-320fc1bb1e15
名前 / ファイル | ライセンス | アクション |
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naltr00260.pdf (1.3 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 | 気流全温度測定装置の試作 | |||||
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 | A High Sensitive Atmospheric Temperature Measuring Apparatus | |||||
著者 |
西尾, 健二
× 西尾, 健二× 能瀬, 弘幸× 越沼, 威× 井上, 重雄× 臼井, 弘× 大畑, 敏美× NISHIO, Kenji× NOUSE, Hiroyuki× KOSHINUMA, Takeshi× INOUE, Shigeo× USUI, Hiroshi× OHATA, Toshimi |
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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 en : Technical Report of National Aerospace Laboratory TR-260 巻 260, p. 11, 発行日 1972-01 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A temperature measuring apparatus for an atmospheric turbulence study which has been made by the Airframe Division and the Flight Research Division of the National Aerospace Laboratory was designed and examined. Ten sets of thermocouples used in a probe are connected in series, and an anti-electro noise amplifier is made which enables us to measure accurately the input signals from the probe installed on an aircraft. The probe has been calibrated in a wind tunnel under the conditions of the flow Mach number ranging from 0.1 to 0.3 and environmental tests in an air at various temperatures ranging from -30C to 30C have been made. Test results showed good characteristics and the apparatus was used for the atmospheric turbulence study. This report contains detailed dimensions of the apparatus and the characteristics obtained from the calibration tests. | |||||
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: NALTR0260000 | |||||
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-260 |