Výsledky vyhledávání - "流れの場"

Numerical simulation of the flow around two Savonius rotors

Autor: Tetsuya, Kawamura

Publikováno v: 紀要 = BULLETIN OF SHIGA BUNKYO JUNIOR COLLEGE. 24:(153)-(165)

垂直軸効力型の風車のひとつにサボニウス風車がある。サボニウス風車には、低速回転、高トルクという特徴があるため、風力発電に用いられることはほとんどないが、最近注目されて�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::b5d528130cddb40d7ecd6c45e33cce5c
http://id.nii.ac.jp/1656/00000103/

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Simulation of virtual flow around an elliptical column in the Riemann surface

Autor: Tetsuya, Kawamura

Publikováno v: 紀要 = BULLETIN OF SHIGA BUNKYO JUNIOR COLLEGE. 24:(139)-(152)

本研究では、どうような状況も作り出せるという数値シミュレーションの利点を活かして、リーマン面内の流体の仮想的な流れのシミュレーションを行った。具体的には２枚のリーマン�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::2a6a555dbb518777cbc6e8caf724f815
http://id.nii.ac.jp/1656/00000102/

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南極周極流南限域における流速構造の変動

Autor: 北出, 裕二郎

東京海洋大学修士学位論文 2019(2020年3月) 海洋資源環境学修士第3311号
指導教員: 渡部和帆
全文公表年月日: 2020-06-22

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::e0c98cdd2120193e08e945dbb82968ff
http://id.nii.ac.jp/1342/00001885/

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Transition and instabilities of flow in a symmetric channel with an expanded and cotracted part

Autor: Inui, Takashi, Shiotani, Yukinobu, Mizushima, Jiro

Publikováno v: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory. 47:81-84

27-28 Sept. 1999 (25th). 27-28 Mar. 2000 (26th)
急な拡大部および縮小部を持つ対称性管路内の流れの遷移と不安定性を2次元非圧縮性流れ場の仮定の下に数値的ならびに理論的に検討した。分岐�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::7c79817277ee2ae9c0570fa51f187fb2
http://id.nii.ac.jp/1696/00041379/

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A Climatological Study on Tropical Cyclone Genesis in the Northwestern Pacific Basin in Sight of Large Scale Flow Field and Merger of Mesoscale Convective Systems

Autor: YOSHIDA, Ryuji, ISHIKAWA, Hirohiko

Publikováno v: 京都大学防災研究所年報. B. 53:345-370

北西太平洋上のメソ対流系の併合を伴った熱帯低気圧(Tropical Cyclone, 以降TCと称す)の発生について，その発生頻度を背景となる環境場別に明らかにするとともに，上層・下層の環境場につ

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::9ec100f8e92d0ca1e04ebc55c5ae1532
http://hdl.handle.net/2433/129391

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有孔フェンス周囲の非定常流れ場の数値シミュレーション

Autor: Takashi Maruyama

Publikováno v: 日本建築学会構造系論文集. 74(639):873-880

Porous fence is an effective device to control the wind flow and to reduce the wind force. The aerodynamic characteristics those necessary to wind resistant design are usually examined by experiment because of the variety of materials and the difficu

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::dc2fc05f99e37eb2111669dc5b888ca8
http://hdl.handle.net/2433/244026

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希薄予混合燃焼器内の燃焼挙動に関する数値解析

Autor: Shinjo, Junji, Matsuyama, Shingo, Mizobuchi, Yasuhiro, Ogawa, Satoru

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2005論文集 = JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2005. :71-75

This study presents numerical simulation results of combustion dynamics in a lean premixed combustor. The combustor is a swirl-stabilized gas turbine model combustor installed at Aerospace Research Center (ARC), Japan Aerospace Exploration Agency (JA

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::b76e3814b2f06ae8bf676490b1565f0d
http://id.nii.ac.jp/1696/00006138/

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Coupled analysis of flowfield and thermal response of ablator under arc-jet flow condition

Autor: Suzuki, Toshiyuki, Yamada, Tetsuya, Sakai, Takeharu, Yamamoto, Yukimitsu

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2005論文集 = JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2005. :88-93

An integrated numerical method to obtain thermal response of ablator under aerodynamic heating environment is briefly described. In this method, a two-dimensional thermal response analysis code, namely SCMA2, is loosely coupled with a thermochemical

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::bb03cfcea572b38bb50cc7339d70797a
http://id.nii.ac.jp/1696/00006141/

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ロケットエンジン同軸型噴射器まわりの燃焼シミュレーション

Autor: Matsuyama, Shingo, Shinjo, Junji, Mizobuchi, Yasuhiro, Ogawa, Satoru

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2005論文集 = JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2005. :65-70

Numerical simulation of liquid oxygen/gaseous hydrogen rocket engine combustor is conducted to investigate the flame structure under supercritical pressure. A preliminary result by an axisymmetric numerical simulation with detailed chemistry is shown

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::4ecbc7c0df06f8c0ff007e1cbcdadbf5
http://id.nii.ac.jp/1696/00006137/

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CFD analyses of shock wave behavior of Busemann's Biplane

Autor: Yamashita, Hiroshi, Yonezawa, Masahito, Goto, Yuichiro, Obayashi, Shigeru, Kusunose, Kazuhiro

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2005論文集 = JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2005. :126-131

Although many kinds of aircrafts are produced, until now, the Concorde is the only supersonic commercial transport (SST) ever built. However, it made its final flight in 2003. It is everyone's dream to be able to go anywhere faster and at the same ti

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::a9614ac2e25453d50860b211e6d9f76e
http://id.nii.ac.jp/1696/00006148/

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