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ALFLEX実験機空力データベースの比較評価
https://jaxa.repo.nii.ac.jp/records/37192
https://jaxa.repo.nii.ac.jp/records/3719288cf1f9f-dac7-4868-bfe4-25909bb57701
名前 / ファイル | ライセンス | アクション |
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nalsp0038010.pdf (1.5 MB)
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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 | ALFLEX実験機空力データベースの比較評価 | |||||
言語 | ||||||
言語 | jpn | |||||
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 | 空力データベース | |||||
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 | ALFLEX | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 自動着陸実験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 動的効果 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 地面効果 | |||||
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 | デルタ翼 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | チップフィン | |||||
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 | aerodynamic database | |||||
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 | ALFLEX | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Automatic Landing Flight Experiment | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | dynamic effect | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | ground effect | |||||
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 | delta wing | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | tip fin | |||||
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 | Evaluation of ALFLEX aerodynamic database | |||||
著者 |
柳原, 正明
× 柳原, 正明× 重見, 仁× 岡田, 典秋× 室田, 勝一× 水藤, 貴靖× Yanagihara, Masaaki× Shigemi, Masashi× Okada, Noriaki× Murota, Katsuichi× Suito, Takanobu |
|||||
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 | ||||||
航空宇宙技術研究所 | ||||||
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 Aerospace Laboratory | ||||||
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. 95-109, 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 | 航空宇宙技術研究所と宇宙開発事業団が共同で実施したHOPE(H-2ロケット打上げ型有翼回収機)小型自動着陸実験(ALFLEX)ではデルタ翼チップフィン形態機の低速空力特性推定が目的の1つとして設定された。ここでは1996年にオーストラリアで実施された飛行試験から動的効果、地面効果も含めたALFLEX実験機の空力特性を推定し、事前に実施されたいくつかの風洞試験の結果と比較評価した。その結果、飛行試験による推定特性と、実験機の制御系設計に使用された基準風洞試験結果との差は概ねバリエーション内であったが、各種風洞試験の間にはかなりのばらつきが見られた。この差の原因としては模型支持方法、模型剛性、模型形状などの違いが考えられる。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | For Automatic Landing Flight Experiment (ALFLEX) conducted jointly by NAL and NASDA using a scale model of HOPE (H-2 Orbiting Plane), the estimation of low-speed aerodynamic characteristics of the delta-wing tip-fin shaped model was aimed as one of the objects. In this report, based on the results of flight tests carried out in Australia 1996, aerodynamic characteristics including both dynamic and ground effects were estimated and compared with the previous results of wind tunnel tests. As a result, the differences were found among different kinds of wind tunnel test, in spite of having found a small difference, almost considered within the extent of variation, between the estimated characteristics from flight tests and the obtained results from tests of standard wind tunnel applied to the design of control system of experimental vehicle. The reason for these differences can be attributed to the difference of supporting method, rigidity, and shape of the model. | |||||
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: AA0001434010 | |||||
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 |