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pro vyhledávání: '"steady aerodynamic simulation"'
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/
