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Recent comparisons of aerothermodynamic results by CFD and FEM coupling analysis with OREX flight experiments
https://jaxa.repo.nii.ac.jp/records/36754
https://jaxa.repo.nii.ac.jp/records/3675498d10e41-8820-4428-b244-066d80bbdf73
名前 / ファイル | ライセンス | アクション |
---|---|---|
nalsp0029004.pdf (958.9 kB)
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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 | ||||||
言語 | en | |||||
タイトル | Recent comparisons of aerothermodynamic results by CFD and FEM coupling analysis with OREX flight experiments | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | OREX | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軌道再突入実験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | CFD | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 計算流体力学 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | FEM | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 有限要素法 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | TPS | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 熱防護系材料 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 非平衡ナビエ・ストークスコード | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 内部熱応答 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 熱伝導効率 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 輻射効果 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 高エンタルピー流れ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空気熱力学データ | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | OREX | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | orbital reentry experiment | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | CFD | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | computational fluid dynamics | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | FEM | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | finite element method | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | TPS | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | thermal protection system | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | nonequilibrium Navier Stokes code | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | internal thermal response | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | heat conduction coefficient | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | radiation effects | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | high enthalpy flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerothermodynamic result | |||||
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 | ||||||
その他のタイトル | CFDとFEMの組合せ解析による空気熱力学データとOREX飛行実験との最近の比較 | |||||
著者 |
山本, 行光
× 山本, 行光× Yamamoto, Yukimitsu |
|||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
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 29, p. 27-39, 発行日 1996-01 |
|||||
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 8 Jun. 1995 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 8 Jun. 1995 Tokyo Japan | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | OREX(軌道再突入実験)のTPS(熱防護系)材料の計測飛行温度データと数値データを比較することによりCFD(計算流体力学)の精度を調べた。非平衡ナビエ・ストークスコードにより流れを計算し、有限要素法(FEM)により内部熱応答を計算した。OREX飛行軌道に沿ってCFD とFEMの組合せで、再突入時のTPSの温度上昇がかなり予測される。FEM解析でTPS材料の温度効果および熱伝導効率と輻射効果の方向依存性が評価される。これらの作業は,NALとNASDAとの共同研究として行われた。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Accuracy of CFD (Computational Fluid Dynamics) is investigated by comparing numerical results with the measured flight temperature data on the TPS (Thermal Protection System) material of OREX (Orbital Reentry Experiments). Flow is calculated by the nonequilibrium Navier-Stokes code and internal thermal response is computed by FEM (Finite Element Method). Coupling CFD and FEM along the OREX flight trajectory, temperature increase of the TPS during reentry is favorably predicted. In FEM analysis, the effects of temperature and directional dependence of heat conduction coefficient and radiation effects of TPS material are evaluated. These works have been done as the joint research of NAL and NASDA. | |||||
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: AA0000110004 | |||||
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-29 |