WEKO3
アイテム
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0.5m極超音速風洞におけるマッハ5及び7 AGARD-B標準模型試験
https://jaxa.repo.nii.ac.jp/records/2587
https://jaxa.repo.nii.ac.jp/records/258785b75cbd-e411-46a6-ba30-13a17534e9b4
名前 / ファイル | ライセンス | アクション |
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64378000.pdf (3.5 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 | 0.5m極超音速風洞におけるマッハ5及び7 AGARD-B標準模型試験 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Force tests, Hypersonic wind tunnel, AGARD calibration model B | |||||
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 | Force tests of an AGARD calibration model B in the JAXA 0.5 m hypersonic wind tunnel at nominal Mach numbers of 5 and 7 | |||||
著者 |
津田, 尚一
× 津田, 尚一× 小山, 忠勇× 平林, 則明× 渡利, 實× 藤井, 啓介× 関根, 英夫× 中村, 晃祥× 木伏, 淳子× Tsuda, Shoichi× Koyama, Tadao× Hirabayashi, Noriaki× Watari, Minoru× Fujii, Keisuke× Sekine, Hideo× Nakamura, Akiyoshi× Kibushi, Junko |
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著者所属 | ||||||
宇宙航空研究開発機構研究開発本部風洞技術開発センター | ||||||
著者所属 | ||||||
宇宙航空研究開発機構研究開発本部風洞技術開発センター | ||||||
著者所属 | ||||||
宇宙航空研究開発機構研究開発本部風洞技術開発センター | ||||||
著者所属 | ||||||
LBM流体力学研究所 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構研究開発本部風洞技術開発センター | ||||||
著者所属 | ||||||
航空宇宙技術振興財団 | ||||||
著者所属 | ||||||
航空宇宙技術振興財団 | ||||||
著者所属(英) | ||||||
en | ||||||
Wind Tunnel Technology Center, Aerospace Research and Development Direstorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Wind Tunnel Technology Center, Aerospace Research and Development Direstorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Wind Tunnel Technology Center, Aerospace Research and Development Direstorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
LBM Computational Fluid Dynamics Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
Wind Tunnel Technology Center, Aerospace Research and Development Direstorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aero-Space Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aero-Space Technology | ||||||
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研究開発資料 en : JAXA Research and Development Memorandum 巻 JAXA-RM-09-001, 発行日 2009-07-31 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 宇宙航空研究開発機構(JAXA)風洞技術開発センターは0.5m極超音速風洞(HWT1)、1.27m極超音速風洞(HWT2)及び0.44m極超音速衝撃風洞(HST)の3つの極超音速風洞を擁している。HWT1では出口直径が0.5mのノズルを交換することによりマッハ数5,7,9の試験が可能である。本稿ではAGARD-B標準模型を用いた6分力試験をHWT1においてマッハ数5及び7で行い、空力特性データを取得したのでその結果を報告する。AGARD-B標準模型は超音速、極超音速領域をカバーする有翼形状の標準模型のひとつであり、国内外の多くの風洞で試験が行われている。マッハ数5の試験結果を他の風洞試験結果と比較し、よく一致することが分かった。他風洞で得られた異なるマッハ数でのデータとの比較においても連続性が認められ、信頼性のある試験結果を得ることができた。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The Wind Tunnel Technology Center (WINTEC) has three hypersonic wind tunnels: the 0.5 m Hypersonic Wind Tunnel (HWT1), the 1.27 m Hypersonic Wind Tunnel (HWT2) and the 0.44 m Hypersonic Shock Tunnel (HST) at the Japan Aerospace Exploration Agency (JAXA). The HWT1 has three interchangeable nozzles with an exit diameter of 0.5 m for Machnumbers of 5, 7 and 9. Force tests were carried out using an AGARD-B calibration model in the HWT1 at nominal Mach numbers of 5 and 7. AGARD-B models have been used as one of the winged calibration models in supersonic and hypersonic wind tunnels. In this report, aerodynamic characteristics of the AGARD-B calibration model at low angles of attack are discussed in Mach 5 and 7 hypersonic flows. Experimental results of Mach 5 showed good agreement with those of other wind tunnels. The data obtained among the HWT1 and other tunnels were correlated well with the free stream Mach number. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-1121 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11983593 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0064378000 | |||||
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-RM-09-001 |