Výsledky vyhledávání - "高レイノルズ数"

Publikováno v: 宇宙航空研究開発機構特別資料: 第39回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2007論文集 = JAXA Special Publication: Proceedings of 39th Fluid Dynamics Conference/Aerospace Numerical Simulation Symposium 2007. :87-90

In the present study, we establish statistical DNS (Direct Numerical Simulation) database in a turbulent channel flow with passive scalar transport at high Reynolds numbers and make the data available at our web site (http://murasun.me.noda.tus.ac.jp

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http://id.nii.ac.jp/1696/00005615/

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Hybrid mesh generation for NAL experimental airplane

Autor: Ito, Yasushi, Nakahashi, Kazuhiro

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). :479-483

SST-CFDワークショップ.次世代超音速機の数値シミュレーション利用技術に関する国際ワークショップ航空宇宙技術研究所 20011203-20011205 東京日本
SST-CFD Workshop. International Workshops on Numer

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http://id.nii.ac.jp/1696/00005785/

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High Reynolds number wind tunnel testing for development of airliners

Autor: Shibata, Makoto

Publikováno v: 宇宙航空研究開発機構特別資料: 第76回風洞研究会議論文集 = JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 76th Meeting. :1-7

資料番号: AA0063330001
レポート番号: JAXA-SP-06-020

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::f603023875ed26bd2a10ce9d8e5a578e
http://id.nii.ac.jp/1696/00005830/

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Local equilibrium of velocity distributions in homogeneous isotropic turbulence

Autor: Tatsumi, Tomomasa, Yoshimura, Takahiro

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. :59-62

Succeeding to the previous reports by the authors which mostly concerned with the inertial similarity of the velocity distributions in homogeneous isotropic turbulence, the local equilibrium similarity of the velocity distributions is studied in this

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::c31eafc7926e95b0fefc786e848c9c6a
http://id.nii.ac.jp/1696/00006195/

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高レイノルズ数乱流場生成ツールとしてのマルチファン型風洞

Autor: Sassa, Koji, Miyagi, Hiromori

We tried to generate quasi-isotropic homogeneous turbulence fields with high Reynolds numbers in the multi-fan wind tunnel. The fans making flow and counter flow were arranged like a checkered pattern and they were driven by a fluctuating signal tran

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::fe1de981db6823540996e0f52457eea0
http://id.nii.ac.jp/1696/00006199/

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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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Experiment on a high Reynolds number turbulent boundary layer

Autor: Fukunishi, Yu, Kohama, Yasuaki, Kobayashi, Ryoji

Publikováno v: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory. 18:25-28

航空宇宙技術研究所 24-25 Sep. 1991 (9th). 16-18 Mar. 1992 (10th) 東京日本
National Aerospace Laboratory 24-25 Sep. 1991 (9th). 16-18 Mar. 1992 (10th) Tokyo Japan
高速鉄道車両の滑らかな屋根を利用して高レイ�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::061da14a787b94f7817d5464af3c0ff3
http://id.nii.ac.jp/1696/00037662/

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高レイノルズ数乱流中の微細コヒーレント構造の検出

Autor: Sassa, Koji

Publikováno v: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory. :61-64

航空宇宙技術研究所 27-29 Sept.2000 東京日本
National Aerospace Laboratory 27-29 Sept.2000 Tokyo Japan
高乱流レイノルズ数がR(sub λ)=280で完全に発達した乱流中の微細コヒーレント渦検出を実験的

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::8270f76eff8764dd52035b341295a45d
http://id.nii.ac.jp/1696/00041402/

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The cryogenic wind tunnel test on HOPE model

Autor: Niwa, Hiroaki, Saito, Katsuya, Nakano, Eiichiro, Aoki, Takeo, Yokomaku, Yoshio

Publikováno v: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory. 42:111-131

21-22 May 1998 (60th). 26-27 Nov. 1998 (61st)
HOPE-X(宇宙往還技術試験機)の実レイノルズ数付近における空力特性データを取得する為に、5%HOPE(H-2ロケット打ち上げ型有翼回収機)風洞試験模型を製

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::b17f2640784f63369d3e4ecea1f08fd5
http://id.nii.ac.jp/1696/00037385/

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非圧縮非有界流れのための4つの開境界条件の有効性の比較

Autor: Hatayama, Shigeki

Publikováno v: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory. :1-28

非圧縮・非有界流れのための4つの開境界条件がLeith型3次精度風上差分法を用いて評価され、その各々の有効性が開境界条件の間の流れの差異および長短の2つの開境界の間の流れの差異�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::22110270ce618a6b4275c9e9b2def917
http://id.nii.ac.jp/1696/00040315/

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