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HOPE極低温高レイノルズ数風洞試験について
https://jaxa.repo.nii.ac.jp/records/37391
https://jaxa.repo.nii.ac.jp/records/373913c183f9f-1d43-40cf-a8ac-966433985547
名前 / ファイル | ライセンス | アクション |
---|---|---|
nalsp0042011.pdf (2.4 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | HOPE極低温高レイノルズ数風洞試験について | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 遷音速風洞 | |||||
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 | 空力特性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 極低温風洞 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | マッハ数 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | クミナル値 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 欧州遷音速風洞株式会社 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | レイノルズ数効果 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | CFD解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 数値流体力学解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 高レイノルズ数 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | HOPE-X | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙往還技術試験機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 6分力天秤 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 有限要素法 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | transonic wind tunnel | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind tunnel | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerodynamic characteristic | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | cryogenic wind tunnel | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Mach number | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | nominal value | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | European Transonic Windtunnel GmbH | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Reynolds number effect | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | CFD analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | computational fluid dynamics analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | high Reynolds number | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | HOPE X | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | H 2 Orbiting Plane Experimental | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | six component balance | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | finite element method | |||||
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 | The cryogenic wind tunnel test on HOPE model | |||||
著者 |
丹羽, 宏明
× 丹羽, 宏明× 齊藤, 勝也× 中野, 英一郎× 青木, 竹夫× 横幕, 良生× Niwa, Hiroaki× Saito, Katsuya× Nakano, Eiichiro× Aoki, Takeo× Yokomaku, Yoshio |
|||||
著者所属 | ||||||
川崎重工業 | ||||||
著者所属 | ||||||
川崎重工業 | ||||||
著者所属 | ||||||
宇宙開発事業団 | ||||||
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 | ||||||
Kawasaki Heavy Industries Ltd | ||||||
著者所属(英) | ||||||
en | ||||||
Kawasaki Heavy Industries Ltd | ||||||
著者所属(英) | ||||||
en | ||||||
National Space Development Agency of Japan | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
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特別資料 en : Special Publication of National Aerospace Laboratory 巻 42, p. 111-131, 発行日 1999-05 |
|||||
会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 21-22 May 1998 (60th). 26-27 Nov. 1998 (61st) | |||||
会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 21-22 May 1998 (60th). 26-27 Nov. 1998 (61st) | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | HOPE-X(宇宙往還技術試験機)の実レイノルズ数付近における空力特性データを取得する為に、5%HOPE(H-2ロケット打ち上げ型有翼回収機)風洞試験模型を製作し、マッハ数0.4〜1.3の風洞試験をETW(欧州遷音速風洞株式会社)で実施した。本レポートは、極低温高レイノルズ数風洞試験用模型の特徴、日本から初めて利用したETW試験設備およびレイノルズ数効果を含めた試験結果について概要を紹介する。また、他風洞試験およびCFD(数値流体力学)解析との結果比較、風洞試験間の誤差について述べる。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A five percent model of HOPE (H-2 Orbiting Plane) was made to obtain the aerodynamic characteristics data near actual Reynolds number for HOPE-X (H-2 Orbiting Plane Experimental), and a wind tunnel test at Mach numbers in the range between 0.4 and 1.3 was conducted at European Transonic Windtunnel GmbH (ETW) in Germany. In this paper, the characteristics of the model for cryogenic high Reynolds number wind tunnel, the outline of test facilities of ETW, which a Japanese team utilized for the first time, and some test results including the Reynolds number effect are reported. These results were compared with those previously obtained in other wind tunnels and those of CFD (Computational Fluid Dynamics) analysis, and the errors between different wind tunnels were discussed. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0289-260X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN10097345 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0001959011 | |||||
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 SP-42 |