Výsledky vyhledávání - "Futatsudera, Naoki"

Some practical applications of CFD analysis to aerodynamic design of the supersonic experimental airplane

Autor: Futatsudera, Naoki, Kaiden, Takeshi

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). :380-389

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
1997年、航空宇宙技術研究所(NAL)は、次世代超音速輸送機開発のための技術的基盤の確立を目�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::ec0f45fb5ab8cbe9b5b7b7c771cef540
http://id.nii.ac.jp/1696/00005770/

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Numerical Simulation of Separated Flows around a Wing Section at Steady and Unsteady Motion by a Discrete Vortex Method

Autor: ASO, Shigeru, FUJIMOTO, Atsushi, FUTATSUDERA, Naoki, HAYASHI, Masanori

Publikováno v: The Institute of Space and Astronautical Science report. S.P. : The Proceedings of the Symposium on Mechanics for Space Flight 1989. 12:15-24

Separated flows around a wing section at fixed attack angle of an oscillating airfoil are simulated numerically by a discrete vortex method combined with a panel method. The potettial flows around wing sections are expressed by vortex sheets and sepa

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::de337f37e7daaa0d7766d9aa038c8c51
http://id.nii.ac.jp/1696/00031205/

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非定常運動をする二次元翼まわりの流れの離散渦法による計算

Autor: Aso, Shigeru, Futatsudera, Naoki, Fujimoto, Atsushi, Hayashi, Masanori

Publikováno v: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory SP-10. 10:27-32

Separated flows around a wing section at unsteady motion are simulated numerically by a discrete vortex method combined with a panel method. The potential flows around wing sections is expressed by vortex sheets and separated shear layers are express

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::4044584f1094d411df4d869f17adb61c
http://id.nii.ac.jp/1696/00043328/

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Numerical Simulation of Separated Flow around Two-Dimensional Wing Section by a Discrete Vortex Method

Autor: ASO, Shigeru, HAYASHI, Masanori, FUTATSUDERA, Naoki

Publikováno v: The Institute of Space and Astronautical Science report. S.P. : The Proceedings of the Symposium on Mechanics for Space Flight 1988. 9:11-20

Separated flows around pitching wing sections are simulated numerically by a discrete vortex method combined with a panal method. The potential flows around wing sections is expressed by vortex sheets and separated shear layers are expressed by discr

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::61b49465685bdb1f233566048e808937
http://id.nii.ac.jp/1696/00031338/

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