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pro vyhledávání: '"3 dimensional flow"'
Autor:
Nakamura, Takashi
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. 57:9-14
The new computer system had been needed to calculate the flow around the wing shape configurations with 1-million gridpoints within ten minutes. And also, it had been needed to get results for full aircraft configurations with 10-million gridpoints w
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::87bdde541b8cc4e38a7ff1d7d8706ed5
http://id.nii.ac.jp/1696/00038217/
http://id.nii.ac.jp/1696/00038217/
Autor:
Ohara, Tsuyoshi, Shima, Eiji
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. 57:100-105
The CFD and thermal coupling analyses system had been developed which software configuration was very compact to need less computational resource named CCAS (Compact Coupling Analyses System). A nodal method was applied for the thermal analyzer in th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::0eb75140e7728ed1c2ec003224b41de3
http://id.nii.ac.jp/1696/00038233/
http://id.nii.ac.jp/1696/00038233/
Publikováno v:
航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory. 57
航空宇宙数値シミュレーション技術シンポジウム2002 航空宇宙技術研究所 20020703-20020705 東京 日本
Aerospace Numerical Simulation Symposium 2002 National Aerospace Laboratory 20020703-20020705 Tokyo Japan
資
Aerospace Numerical Simulation Symposium 2002 National Aerospace Laboratory 20020703-20020705 Tokyo Japan
資
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::caec944ce7fd3cdb73f3bc395420b698
http://id.nii.ac.jp/1696/00038215/
http://id.nii.ac.jp/1696/00038215/
Autor:
Nishizawa, Akira, Takagi, Shohei
Publikováno v:
航空宇宙技術研究所特別資料: 境界層遷移の解明と制御研究会講演論文集 第29回・第30回 = Special Publication of National Aerospace Laboratory: Proceedings of the 29th and 30th NAL Workshops on Investigation and Control of Boundary-Layer Transition. 56:93-94
Characteristic features of a wave packet in a rotating-disk boundary layer were experimentally investigated. The point disturbance originating from a small hole on the disk forms an isolated wave packet which consists of two types of unstable waves.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::0ea0ac9eb5eec7e667b039a839b70251
http://id.nii.ac.jp/1696/00038214/
http://id.nii.ac.jp/1696/00038214/
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