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傾斜型熱線流速計による軸流圧縮機内部の3次元計測
https://jaxa.repo.nii.ac.jp/records/44858
https://jaxa.repo.nii.ac.jp/records/44858be7423fc-a1c3-4cc3-b0a6-45ffb2da26b2
名前 / ファイル | ライセンス | アクション |
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naltr00603.pdf (848.5 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 | 傾斜型熱線流速計による軸流圧縮機内部の3次元計測 | |||||
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 | Three Dimensional Flow Measurement in the Axial Compressor with a Single Slanted Hot-Wire | |||||
著者 |
熊谷, 隆王
× 熊谷, 隆王× 田中, 英穂× 丸田, 秀雄× KUMAGAI, Takao× TANAKA, Hideho× MARUTA, Hideo |
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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 | ||||||
東京大学宇宙航空研究所 | ||||||
著者所属 | ||||||
東京大学宇宙航空研究所 | ||||||
著者所属(英) | ||||||
en | ||||||
Aeroengine Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Aeronautical Science, The University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Aeronautical Science, The University of Tokyo | ||||||
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-603 巻 603, p. 11, 発行日 1980-02 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | To measure three-dimensional air flow in the axial flow compressors, several kinds of slanted hot-wire anemometery techniques have been developed in recent years. Quick response and less disturbance to the flow are the typical advantages of this method of measurement. In our experiment, the measuring system consists of a hot-wire anemometer with a single slanted wire probe and a data processing system. Exit flow of the axial flow compressor with 15 rotor blades is measured by the system. The anemometer output signals, obtained by locating a probe at three positions in each 120deg orientations, are sampled, averaged and calculated using the directional consines techinque. The resulting processing data show the values for three-dimensional components of mean velocity, swirl angle and pitch angle. The decay and the diffusion of the rotor wakes are also presented. | |||||
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: NALTR0603000 | |||||
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-603 |