Zobrazeno 1 - 10 of 20 pro vyhledávání: '"UPACS"'
1
CFD analyses of shock wave behavior of Busemann's Biplane
Autor: Yamashita, Hiroshi, Yonezawa, Masahito, Goto, Yuichiro, Obayashi, Shigeru, Kusunose, Kazuhiro
Publikováno v: 宇宙航空研究開発機構特別資料: 航空宇宙数値シミュレーション技術シンポジウム2005論文集 = JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2005. :126-131
Although many kinds of aircrafts are produced, until now, the Concorde is the only supersonic commercial transport (SST) ever built. However, it made its final flight in 2003. It is everyone's dream to be able to go anywhere faster and at the same ti
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::a9614ac2e25453d50860b211e6d9f76e
http://id.nii.ac.jp/1696/00006148/
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3
Report and comments about the panel discussion present status and challenges of computer science
Autor: Kubota, Hirotoshi
Publikováno v: 宇宙航空研究開発機構特別資料: 航空宇宙数値シミュレーション技術シンポジウム2006論文集 = JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2006. :29-37
2006年6月23日、如水会館において、(独)宇宙航空研究開発機構の主催により「航空宇宙数値シミュレーション技術シンポジウム2006」が開催された。その中で、同日17:00-18:00に標記のパネル
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::b47303f3dacd13079b1a6300de3677da
http://id.nii.ac.jp/1696/00005945/
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4
Validation study for turbulence models implemented in UPACS
Autor: Ito, Ryozo, Imamura, Taro
Publikováno v: 宇宙航空研究開発機構特別資料: 航空宇宙数値シミュレーション技術シンポジウム2005論文集 = JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2005. :11-16
The SST (Shear-Stress Transport) turbulence model has been implemented in UPACS, a CFD platform developed in JAXA. Four test cases with increasing level of difficulty were used to validate the present implementation. Three basic test cases included f
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::bef396fc2d3c34ff31fd98391b2c3c3f
http://id.nii.ac.jp/1696/00006128/
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5
Improvement of the domain connectivity database tool for overset grid simulations using UPACS
Autor: Matsumura, Yosuke, Higashida, Akihiro, Murakami, Hiroyuki, Yamane, Takashi, Takaki, Ryoji, Yamamoto, Kazuomi
Publikováno v: 宇宙航空研究開発機構特別資料: 航空宇宙数値シミュレーション技術シンポジウム2004論文集 = JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2004. :248-253
UPACS (Unified Platform for Aerospace Computational Simulation), which aims to be a common CFD platform, is a solver for compressible flows around complicated geometries using the multi-block structured grid method. In order to ease application to mo
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::46327990f1427dedcfe42790504041d5
http://id.nii.ac.jp/1696/00006476/
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6
Flow simulation using a hybrid of Cartesian and prismatic grids
Autor: Lahur, Paulus
Publikováno v: 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2002論文集 = Special Publication of National Aerospace Laboratory: Proceedings of Aerospace Numerical Simulation Symposium 2002. 57:249-252
This paper discusses the current development of a hybrid grid method suitable for compressible and viscous flow simulation. The method is part of computational software platform, UPACS (Unified Platform for Aerospace Computational Simulation), being
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::d5e6c8f81bc5261e5dd23eb47472bb5a
http://id.nii.ac.jp/1696/00038259/
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7
Coupled simulation of flow and heat conduction by UPACS
Autor: Yamane, Takashi, Enomoto, Shunji, Takaki, Ryoji, Yamamoto, Kazuomi
Publikováno v: 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2002論文集 = Special Publication of National Aerospace Laboratory: Proceedings of Aerospace Numerical Simulation Symposium 2002. 57:124-129
UPACS, Unified Platform for Aerospace Computational Simulation, is a project to develop a common CFD platform since 1998 at National Aerospace Laboratory of Japan. The project aims not only to overcome the increasing difficulty in recent CFD code pro
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::87723fbb0de1e743508c8485232e29c4
http://id.nii.ac.jp/1696/00038237/
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8
Numerical simulation of 2D airfoil stall by UPACS: CFD Workshop on 2D airfoil stall predict
Autor: Takaki, Ryoji, Yamamoto, Kazuomi, Enomoto, Shunji, Yamazaki, Hiroyuki, Yamane, Takashi, Iwamiya, Toshiyuki
Publikováno v: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory. 46:163-168
航空宇宙技術研究所 7-9 Jun. 2000 東京 日本
National Aerospace Laboratory 7-9 Jun. 2000 Tokyo Japan
3種類の2次元翼の静的失速現象について数値的に調べた。UPACS(航空宇宙計算シミュレーション統
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::e9470f25fa2d171e397c5da816efdcc2
http://id.nii.ac.jp/1696/00041325/
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9
Current status of common CFD platform-UPACS
Autor: Yamane, Takashi, Yamamoto, Kazuomi, Enomoto, Shunji, Takaki, Ryoji, Yamazaki, Hiroyuki, Makida, Mitsumasa, Yamamoto, Takeshi, Iwamiya, Toshiyuki, Nakamura, Takashi
Publikováno v: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory. 46:45-50
航空宇宙技術研究所 7-9 Jun. 2000 東京 日本
National Aerospace Laboratory 7-9 Jun. 2000 Tokyo Japan
UPACS(航空宇宙計算シミュレーション統一基準)は、共通的なCFD(計算流体力学)プラットフォーム
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::9fbdd96a379c08f47fbdef091b299b42
http://id.nii.ac.jp/1696/00041304/
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10
超音速輸送機周りの流れをシミュレーションする構造格子法
Autor: Enomoto, Shunji
Publikováno v: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory. :213-216
航空宇宙技術研究所 17-19 Jan. 2000 東京 日本
National Aerospace Laboratory 17-19 Jan. 2000 Tokyo Japan
NALのSST(超音速輸送機)プロジェクトにおいて、機体およびエンジンの周りの複雑な流れを高
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::189a0739db37651a521da825a20ff32f
http://id.nii.ac.jp/1696/00041441/
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