WEKO3
アイテム
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並列計算機による時間変動成分を考慮した乱流燃焼解析ソフトウェアの開発:2次元予混合火炎バーナーの解析
https://jaxa.repo.nii.ac.jp/records/38088
https://jaxa.repo.nii.ac.jp/records/380884d667a57-50d5-41d2-8137-8617d05b64d6
名前 / ファイル | ライセンス | アクション |
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nalsp0053051.pdf (3.3 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 | 並列計算機による時間変動成分を考慮した乱流燃焼解析ソフトウェアの開発:2次元予混合火炎バーナーの解析 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 乱流燃焼 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 乱流 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | パラレルコンピューティング | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 数値解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 圧縮性流体 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 亜音速流 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | エネルギー保存則 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | turbulent combustion | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | turbulent flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | parallel computing | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | numerical simulation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | compressible flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | subsonic flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | energy conservation | |||||
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 | Development of a turbulent combustion analysis code treating dynamical turbulent flow for parallel computing | |||||
著者 |
牧田, 光正
× 牧田, 光正× 林, 茂× 川名, 輝子× 筧, 雅行× 小池, 秀耀× 小林, 敏雄× 谷口, 伸行× Makida, Mitsumasa× Hayashi, Shigeru× Kawana, Teruko× Kakei, Masayuki× Koike, Hideaki× Kobayashi, Toshio× Taniguchi, Nobuyuki |
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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 | ||||||
富士総合研究所 | ||||||
著者所属 | ||||||
富士総合研究所 | ||||||
著者所属 | ||||||
富士総合研究所 | ||||||
著者所属 | ||||||
東京大学 | ||||||
著者所属 | ||||||
東京大学 | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
Fuji Research Institute Corporation | ||||||
著者所属(英) | ||||||
en | ||||||
Fuji Research Institute Corporation | ||||||
著者所属(英) | ||||||
en | ||||||
Fuji Research Institute Corporation | ||||||
著者所属(英) | ||||||
en | ||||||
University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
University of Tokyo | ||||||
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: 航空宇宙数値シミュレーション技術シンポジウム2001論文集 en : Special Publication of National Aerospace Laboratory: Proceedings of Aerospace Numerical Simulation Symposium 2001 巻 53, p. 303-308, 発行日 2002-01 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A turbulent combustion analysis code is being developed for large scale numerical simulation of combustion phenomena using parallel computing machines. In this study the following calculations were made. Firstly, zero Mach number approximation is applied to the analysis of subsonic compressible flow, and BFC coordinate is taken for considering the real complicated shape of the burner. Secondly, the stabilization of the simulation including various time scales is realized by coupling equation of continuity with equation of energy conservation via equation of state. The result of LES simulation shows that it is qualitatively valid for the real combustion phenomena. | |||||
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: AA0032819052 | |||||
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-53 |