WEKO3
アイテム
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流体・壁面後退量連成解析によるノズル壁後退量評価
https://jaxa.repo.nii.ac.jp/records/2139
https://jaxa.repo.nii.ac.jp/records/2139141257b5-594c-47b1-b5f0-a2e50b85b935
名前 / ファイル | ライセンス | アクション |
---|---|---|
63804000.pdf (1.7 MB)
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|
Item type | テクニカルレポート / Technical Report(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 流体・壁面後退量連成解析によるノズル壁後退量評価 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ノズル設計 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ノズル流 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ノズル形状 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ロケットノズル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | スロート | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 炭素繊維強化樹脂 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | アブレーション材料 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | アブレーション | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ノズル壁 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 後退 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 固体ロケット推進薬 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 推進薬燃焼 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 計算機シミュレーション | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | nozzle design | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | nozzle flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | nozzle geometry | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | rocket nozzle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | throat | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | carbon fiber reinforced plastic | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | ablative material | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | ablation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | nozzle wall | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | recession | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | solid rocket propellant | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | propellant combustion | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | computerized simulation | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Estimation of recession amount of nozzle wall using coupled fluid/thermochemical approach | |||||
著者 |
大門, 優
× 大門, 優× 嶋田, 徹× 坪井, 伸幸× 高木, 亮治× 藤田, 和央× 竹川, 国之× Daimon, Yu× Shimada, Toru× Tsuboi, Nobuyuki× Takaki, Ryoji× Fujita, Kazuhisa× Takekawa, Kuniyuki |
|||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 宇宙輸送工学研究系 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 宇宙輸送工学研究系 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 宇宙輸送工学研究系 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 宇宙科学研究本部 宇宙科学情報解析センター | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 空気力学研究グループ | ||||||
著者所属 | ||||||
菱友システムズ エンジニアリングソリューション事業部 | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Department of Space Transportation Engineering, Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Department of Space Transportation Engineering, Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Department of Space Transportation Engineering, Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Center for Planning and Information Systems, Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Aerodynamics Research Group, Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Ryoyu Systems Co. Ltd. Engineering Solution Division | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構 | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構研究開発報告 en : JAXA Research and Development Report 巻 JAXA-RR-07-035, 発行日 2008-02-29 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Evaluation of ablation of nozzle wall in solid rocket motor is studied numerically on three solid rocket motors. A coupled analysis of fluid dynamics and surface recession simulates a total ablation amount. The analysis consists of the two-dimensional axisymmetric fluid analysis and the estimation of ablation amount using a correlation equation of surface recession rate. The simulation results of total surface recession amount agree qualitatively with experimental results in Nozzle-A case. The numerical simulations estimate the erosion rate on the safe-side. The effect of shield for reactant gas from nozzle surface reaction is estimated by a simple model. This model works very well for the agreement to experimental results. However, the parameter of the model has to be decided from experimental data. This model is not sufficient for prediction of unknown rocket motor. The coupled analysis was performed on Nozzle-B and C cases in order to understand flow field and erosion mechanism. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-1113 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA1192675X | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0063804000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-RR-07-035 |