Zobrazeno 1 - 6 of 6 pro vyhledávání: '"Navier Stokes equations numerical solution"'
1
Comparison between experiment and computation for the near wake behind a circular cylinder
Autor: Otaguro, Toshio, Suito, Hiroshi
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11回・第12回) = Proceedings of the 11th and 12th NAL Workshop on 'Investigation and Control of Boundary-Layer Transition'. Special Publication of National Aerospace Laboratory. 21:25-29
航空宇宙技術研究所 28-29 Sep. 1992. 25-26 Apr.1993 東京 日本
National Aerospace Laboratory 28-29 Sep. 1992. 25-26 Apr.1993 Tokyo Japan
実験と計算機流体力学解析(CFD)の間の密接な連携の可能性を試す目的
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::28142f08eabfbd1ef84c5c691139faaa
http://id.nii.ac.jp/1696/00037737/
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2
Numerical simulation of laminar-turbulent transition in a rectangular duct flow
Autor: Yamada, Tatsuya, Hosokawa, Iwao, Yamamoto, Kiyoshi
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11回・第12回) = Proceedings of the 11th and 12th NAL Workshop on 'Investigation and Control of Boundary-Layer Transition'. Special Publication of National Aerospace Laboratory. 21:5-8
航空宇宙技術研究所 28-29 Sep. 1992. 25-26 Apr.1993 東京 日本
National Aerospace Laboratory 28-29 Sep. 1992. 25-26 Apr.1993 Tokyo Japan
スペクトル法を用いて、矩形ダクト内の流れにおける層流から乱流
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::2ab73fcfa3c4f3a4e993d8ed2e5e09a1
http://id.nii.ac.jp/1696/00037733/
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3
Computations of unsteady aerodynamic loads around oscillating wings. Part 1: Formulation
Autor: Nakamichi, Jiro
Publikováno v: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory. 1202:1-21
空力弾性の分野では、従来非粘性モデルの非定常空気力が用いられてきたが、ストール/フラッター、バッフェット、バズなど、流れの粘性に起因する現象の解析的研究の目的からも、粘
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::62929f08d2558f0e7e8a31e724a7aac3
http://id.nii.ac.jp/1696/00041181/
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4
Large-Eddy Simulations of Molecular Mixing in a Recirculating Shear Flow
Autor: Matheou, Georgios
The flow field and mixing in an expansion-ramp geometry is studied using large-eddy simulation (LES) with subgrid scale (SGS) modeling based on the stretched-vortex model. The expansionramp geometry was developed to provide enhanced mixing and flameh
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::4efadb5e5c008b50ad91a8033f03fd2d
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5
Absolute and convective chaos in a wake
Autor: Maekawa, Hiroshi
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11回・第12回) = Proceedings of the 11th and 12th NAL Workshop on 'Investigation and Control of Boundary-Layer Transition'. Special Publication of National Aerospace Laboratory. 21:55-57
航空宇宙技術研究所 28-29 Sep. 1992. 25-26 Apr.1993 東京 日本
National Aerospace Laboratory 28-29 Sep. 1992. 25-26 Apr.1993 Tokyo Japan
本論文では、空間的に発達する2次元後流の直接シミュレーションを
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::a5ce736a6f0e18cb95b203345c88f3d6
http://id.nii.ac.jp/1696/00037744/
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