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Numerical simulation of the internal flow through the Mach 2 air-intake designed for NAL's experimental airplane

Publikováno v: 宇宙航空研究開発機構特別資料 = JAXA Special Publication: Proceedings of International Workshops on Numerical Simulation Technology for Design of Next Generation Supersonic Civil Transport (SST-CFD Workshop). :173-179

SST-CFD Workshop. International CFD Workshops for Super-sonic Transport Design 航空宇宙技術研究所 19980316-19980317 東京日本
SST-CFD Workshop. International CFD Workshops for Super-sonic Transport Design National Aerospace Laborato

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::d61913c1b08553d5e0638de328e6078d
http://id.nii.ac.jp/1696/00005744/

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CFD analysis applied to the supersonic research airplane

Autor: Takaki, Ryoji, Iwamiya, Toshiyuki, Aoki, Akiko

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::89ba76614b63a44e374d5bae4852305b
http://id.nii.ac.jp/1696/00005736/

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Control of oscillatory thermocapillary convection

Autor: Shiomi, Junichiro

Publikováno v: 宇宙航空研究開発機構特別資料: 境界層遷移の解明と制御研究会講演論文集第35回・第36回 = JAXA Special Publication: Proceedings of the 35th and 36th JAXA Workshops on Investigation and Control of Boundary-Layer Transition. :47-50

Possibility to stabilize the oscillatory thermocapillary convection is demonstrated using a proportional feedback control. The feedback control is realized by locally modifying the surface temperature by using the local temperature measured at differ

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::5081f86dbf69488f0cc4f25c52bd282f
http://id.nii.ac.jp/1696/00006191/

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Simulation of a flow around an airfoil with a circulation boundary condition

Autor: Kuwahara, Kunio, Komurasaki, Satoko

In the present paper, a simulation of a subsonic flow around airfoil NACA0012 is attacked. Computations are done at angles of attack 8 deg to 18 deg and at the Reynolds number of 106 based on the chord length. In this computation, the incompressible

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::653354884421dc08a484d1ec52e16762
http://id.nii.ac.jp/1696/00006190/

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A three-dimensional MHD analysis for a Magneto Plasma Sail

Autor: Nagata, Yasunori, Otsu, Hirotaka

Publikováno v: 宇宙航空研究開発機構研究開発報告: 磁気プラズマセイルの推力発生メカニズムの解明 = JAXA Research and Development Report: Elucidation of Thrust Generation Mechanism of Magnetic Sail. :9-16

磁気プラズマセイル(Magneto Plasma Sail, MPS)とは外惑星探査用の推進システムであり、太陽から放射されている太陽風を、機体の周りに発生させた磁場で受け止めることで推力を発生させる�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::4f4c53508158b81750f8f888068d559c
http://id.nii.ac.jp/1696/00002273/

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Numerical simulation of unsteady three-dimensional flow field in a turbine stage

Autor: Yamada, Kazutoyo, Funazaki, Kenichi, Hiroma, Kazuto, Tsutsumi, Masanori, Hirano, Yuichiro

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. :166-171

In present study, the unsteady effect of rotor-stator interaction on turbine stage performance was investigated. Unsteady RANS simulations were performed to clarify the unsteady three-dimensional flow field in a turbine stage. Concerning the flow fie

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::e0390384f4a51617435bf7a83e62d311
http://id.nii.ac.jp/1696/00006462/

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History of NWT from 1993

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/

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New compact coupling analyses system with 3-D CFD solver & thermal analyzer with nodal method

Autor: Ohara, Tsuyoshi, Shima, Eiji

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/

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Feasibility of large eddy simulation of turbulent flows for engineering application

Autor: Taniguchi, Nobuyuki

Publikováno v: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory. 44:291-296

航空宇宙技術研究所 16-18 Jun. 1999 東京日本
National Aerospace Laboratory 16-18 Jun. 1999 Tokyo Japan
乱流の予測は、流体機械設計において重要な問題であるが、特に、流れの剥離にしばしば関�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::0b13c331ca3bd6734b1b964a58d205ed
http://id.nii.ac.jp/1696/00037473/

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渦・衝撃波干渉の数値計算

Autor: Hashiguchi, Masanori

Publikováno v: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory. 40:11-14

30 Sep.-1 Oct. 1997 (21st). 26-27 Mar. 1998 (22nd)
垂直衝撃波と縦渦との干渉を、圧縮性オイラー方程式を解くことによって数値的に調べた。軸対称3次元流を仮定した。その支配方程式を、有限�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::3322c11874518ce244aba28dcf6fa4fe
http://id.nii.ac.jp/1696/00037220/

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