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07HOPE遷音速対応風洞試験
https://jaxa.repo.nii.ac.jp/records/37194
https://jaxa.repo.nii.ac.jp/records/37194917efbb3-436a-4451-a37c-09adf8798e51
名前 / ファイル | ライセンス | アクション |
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nalsp0038012.pdf (816.7 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 | 07HOPE遷音速対応風洞試験 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | HOPE | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | H-2ロケット打上げ型有翼回収機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空力係数誤差 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | トレランス | |||||
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 | 遷音速風洞 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 対応風洞試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 縮尺比 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | HOPE | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | H 2 orbiting plane | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerodynamic coefficient error | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | torelance | |||||
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 | transonic wind tunnel | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | comparing wind tunnel test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | scale ratio | |||||
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 second estimations of wind tunnel uncertainties for HOPE | |||||
著者 |
青木, 竹夫
× 青木, 竹夫× 鈴木, 弘一× 中村, 正剛× 若松, 逸雄× 中野, 英一郎× Aoki, Takeo× Suzuki, Koichi× Nakamura, Seigo× Wakamatsu, Itsuo× Nakano, Eiichiro |
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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 | ||||||
宇宙開発事業団 | ||||||
著者所属 | ||||||
宇宙開発事業団 | ||||||
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 | ||||||
著者所属(英) | ||||||
en | ||||||
National Space Development Agency of Japan | ||||||
著者所属(英) | ||||||
en | ||||||
National Space Development Agency of Japan | ||||||
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 38, p. 139-153, 発行日 1998-01 |
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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 | 22-23 May 1997 (58th). 27-28 Nov. 1997 (59th) | |||||
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 | 22-23 May 1997 (58th). 27-28 Nov. 1997 (59th) | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 宇宙往還技術試験機の空力係数誤差を設定する作業の一環として06HOPE(H-2ロケット打上げ型有翼回収機)模型による対応風洞試験に続き、07HOPE模型を使用して同じ方法で対応風洞試験を行った。06および07の対応風洞試験結果はCn(sub β)の差のピークでは3倍異なったが、この他の差は、ほぼ同じレベル・同じ傾向を示した。また、今回は新たな別の試験結果も加えて、試験結果間の差の縮小の可能性についても議論する。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | As a part of work for setting aerodynamic coefficient errors of experimental vehicle for reusable space transportation, corresponding wind tunnel comparing test on 07HOPE (H-2 Orbiting Plane) model was carried out in the same manner as the preceding test on 06HOPE. The results of comparing tests on the 06 and 07HOPE model showed that the peak of difference of Cn(sub beta) of 07HOPE model is three times as large as that of 06, but other differences were roughly in the same level and tendency. Further in this time, adding other new test results, the possibility of diminishing differences among test results is 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: AA0001434012 | |||||
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-38 |