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2次元Jet-In-Cross Flowにおける時間変動場抑制に向けた形状最適化問題
https://jaxa.repo.nii.ac.jp/records/48388
https://jaxa.repo.nii.ac.jp/records/483886bd96553-e33d-4e50-a54f-410d303a8ed9
名前 / ファイル | ライセンス | アクション |
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AA2130027015.pdf (2.6 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2022-02-14 | |||||
タイトル | ||||||
タイトル | 2次元Jet-In-Cross Flowにおける時間変動場抑制に向けた形状最適化問題 | |||||
言語 | ||||||
言語 | jpn | |||||
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 | Shape Optimization Problem for Time Fluctuation Velocity Fields of the Two-Dimensional Jet-In-Cross Flow | |||||
著者 |
中澤, 嵩
× 中澤, 嵩× 三坂, 孝志× NAKAZAWA, Takashi× MISAKA, Takashi |
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著者所属 | ||||||
大阪大学数理・データ科学教育研究センター(MMDS) | ||||||
著者所属 | ||||||
産業技術総合研究所(AIST) | ||||||
著者所属(英) | ||||||
en | ||||||
Center for Mathematical Modeling and Data Science, Osaka University (MMDS) | ||||||
著者所属(英) | ||||||
en | ||||||
National Institute of Advanced Industrial Science and Technology (AIST) | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構(JAXA) | |||||
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特別資料: 第53回流体力学講演会/第39回航空宇宙数値シミュレーション技術シンポジウム論文集 en : JAXA Special Publication: Proceedings of the 53rd Fluid Dynamics Conference / the 39th Aerospace Numerical Simulation Symposium 巻 JAXA-SP-21-008, p. 175-183, 発行日 2022-02-14 |
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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 | 第53回流体力学講演会/第39回航空宇宙数値シミュレーション技術シンポジウム (2021年6月30日-7月2日. 日本航空宇宙学会 : 宇宙航空研究開発機構(JAXA)オンライン会議) | |||||
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 | The 53rd Fluid Dynamics Conference / the 39th Aerospace Numerical Simulation Symposium (June 30 - July 2, 2021. The Japan Society for Aeronautical and Space Sciences : Japan Aerospace Exploration Agency (JAXA), Online meeting) | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | This paper presents a versatile and Snapshot POD-based shape optimization method, to delay laminar-turbulent transition and to promote a mixing. The main problem is the nonstationary Navier-Stokes problem and eigenvalue problem for Snapshot POD, ad more the eigenvalues of Snapshot POD is defined as the cost function. Based on Lagrange multiplier method, the objective cost functional is obtained, and by using Adjoint variable method main problem and adjoint problems are solved to evaluate the sensitivity. The two-dimensional Jet-In-Cross flow used as an initial domain is reshaped iteratively. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
ISSNONLINE | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 2433-2232 | |||||
著者版フラグ | ||||||
出版タイプ | VoR | |||||
出版タイプResource | http://purl.org/coar/version/c_970fb48d4fbd8a85 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA2130027015 | |||||
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-SP-21-008 |