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ジェット実験機インテークの超音速風洞試験
https://jaxa.repo.nii.ac.jp/records/6598
https://jaxa.repo.nii.ac.jp/records/6598dc0e46f2-49ef-45a3-93bc-e0c4a085384a
名前 / ファイル | ライセンス | アクション |
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47428009.pdf (575.0 kB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | ジェット実験機インテークの超音速風洞試験 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 超音速風洞 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風洞試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風洞模型 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ジェット航空機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | エアインテーク | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 外部圧縮型インテーク | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 流量計校正 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 気流特性 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | supersonic wind tunnel | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind tunnel test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind tunnel model | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | jet aircraft | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | air intake | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | external compression intake | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flowmeter calibration | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flow characteristic | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Supersonic wind tunnel test of air-intake for the jet-powered experimental airplane | |||||
著者 |
渡辺, 安
× 渡辺, 安× 村上, 哲× 藤原, 仁志× Watanabe, Yasushi× Murakami, Akira× Fujiwara, Hitoshi |
|||||
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(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構 | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構特別資料: 第66回 風洞研究会議論文集 en : JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 66th Meeting 巻 JAXA-SP-03-003, p. 81-84, 発行日 2004-03-25 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Supersonic wind tunnel test of the air intake for the jet-powered experimental airplane was conducted associated with the NAL SST project. In order to estimate the supercritical and subcritical operation margin, the short compact mass flow meter with high accuracy is required in the wind tunnel test. Such a compact mass flow meter was designed and applied to the wind tunnel test. However, the result of wind tunnel test indicates that there is some problems associated with the calibration of the mass flow meter to achieve high accuracy. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-113X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11984031 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0047428009 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-SP-03-003 |