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極超音速飛行実験(HYFLEX)機のCFD解析
https://jaxa.repo.nii.ac.jp/records/37779
https://jaxa.repo.nii.ac.jp/records/3777993920fc1-39a9-49aa-9ae6-e2f21f7d53d8
名前 / ファイル | ライセンス | アクション |
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nalsp0022018.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 | 極超音速飛行実験(HYFLEX)機のCFD解析 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | HYFLEX | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 極超音速飛行実験機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 極超音速空力特性 | |||||
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 | 極超音速風洞試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 極超音速舵効き | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | スペースプレーン | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空力加熱特性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ボディフラップ形態 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 流れ数値シミュレーション | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ナビエ・ストークス方程式数値解 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | CFD応用 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | CFD対風洞相関 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 双曲的格子形成 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | HYFLEX | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | HYpersonic FLight EXperiment vehicle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | hypersonic aerodynamic characteristic | |||||
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 | hypersonic wind tunnel test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | hypersonic control surface effectiveness | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | spaceplane | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerodynamic heating characteristic | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | body flap configuration | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | numerical flow simulation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Navier Stokes equation numerical solution | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | CFD application | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | CFD wind tunnel correlation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | hyperbolic grid generation | |||||
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 | Numerical simulation of hypersonic flight experiment vehicle | |||||
著者 |
山本, 行光
× 山本, 行光× 吉岡, 美菜子× Yamamoto, Yukimitsu× Yoshioka, Minako |
|||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
富士通 | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
FUJITSU LIMITED | ||||||
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: 第11回航空機計算空気力学シンポジウム論文集 en : Special Publication of National Aerospace Laboratory: Proceedings of the 11th NAL Symposium on aircraft computational aerodynamics 巻 22, p. 109-114, 発行日 1994-03 |
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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 | 航空宇宙技術研究所 10-11 Jun. 1993 東京 日本 | |||||
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 | National Aerospace Laboratory 10-11 Jun. 1993 Tokyo Japan | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 極超音速飛行実験機(HYFLEX)の極超音速空力特性を航技研(NAL)のナビエ・ストークスCFD(計算空気力学)コードを用いた数値シミュレーションにより調べた。数値解析結果をNAL極超音速風洞で得られた実験データと比較した。実飛行時の空力特性を調べるため、空力加熱の最も厳しい飛行条件に対応する数値計算も行い、飛行条件と風洞試験条件の差を考察した。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Hypersonic aerodynamic characteristics of Hypersonic FLight EXperiment (HYFLEX vehicle were investigated by numerical simulations using Navier-Stokes CFD (Computational Fluid Dynamics) code of NAL. Numerical results were compared with experimental data obtained at Hypersonic Wind Tunnel at NAL. In order to investigate real flight aerodynamic characteristics. numerical calculations corresponding to the flight conditions suffering from maximum aero thermodynamic heating were also made and the differences between flight and experimental conditions were considered. | |||||
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: AA0004171019 | |||||
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-22 |