Výsledky vyhledávání - "Koshioka, Yasuhiro"

Simulation technology in Fuji Heavy Industries: Today and in the future

Autor: Koshioka, Yasuhiro

Publikováno v: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory. 46:85-88

航空宇宙技術研究所 7-9 Jun. 2000 東京日本
National Aerospace Laboratory 7-9 Jun. 2000 Tokyo Japan
産業用ロボットを用いて風洞内における特定の航空機に適用する制御則を容易に評価するため�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::d8888a5fa536cbaeb8c417cd50b24bb6
http://id.nii.ac.jp/1696/00041311/

Zobrazit plný text záznamu

An experimental and numerical study on supersonic boundary layer: Stability and transition prediction

Autor: Koshioka, Yasuhiro, Tani, Yasuhiro, Yoshida, Shigeo

Publikováno v: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory. 36:37-40

航空宇宙技術研究所 26-28 Mar. 1997 東京日本
National Aerospace Laboratory 26-28 Mar. 1997 Tokyo Japan
超音速境界層安定性および遷移予測に関する風洞試験と安定性解析を行った。後退角が45度�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::473a07aaf618c01bbe19260406f77653
http://id.nii.ac.jp/1696/00037094/

Zobrazit plný text záznamu

Overview of DREAMS Project

Autor: Koshioka, Yasuhiro

Publikováno v: 日本航空宇宙学会誌 = Aeronautical and Space Sciences Japan. 64(5):135(7)-139(11)

経済成長著しいアジア諸国を中心に航空需要が増加し，2030年には世界の航空交通量が現在のおよそ2倍になると予想されている．運航数の増加は旅客の利便性向上へとつながるが，他方�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::affac073d8ef6af27e9c0767986b2540
http://id.nii.ac.jp/1696/00021694/

Zobrazit plný text záznamu

Numerical calculation of non-equilibrium flow around two-dimensional axisymmetric OREX

Autor: Matsumoto, Takashi, Yamauchi, Toyosei, Koshioka, Yasuhiro, Kiyoshima, Satosi

Publikováno v: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory. 26:67-70

非平衡層流であるOREXのまわりの2次元軸対称極超音速流を数値的に計算した。強い衝撃波を含む極超音速流を安定に解くために、Roeの流束差分分割法に基く風上差分解法を採用した。気�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::e20073ef1f1ee211da206be8ec92c8a4
http://id.nii.ac.jp/1696/00037829/

Zobrazit plný text záznamu

Description of 2D problem: Aerodynamic analysis of Garabedian-Korn 75-06-12 airfoil

Autor: Sakya, A.E., Hirose, Naoki, Sakya, Andi Eka, Nakamura, Yoshiaki, Higaki, Kyoko, Koshioka, Yasuhiro, Shima, Eiji, Egami, Koichi, Nishikawa, Nobuhide, Matsushima, Kisa, Kaiden, Takeshi

Publikováno v: 航空宇宙技術研究所特別資料: 第10回航空機計算空気力学シンポジウム論文集特別企画/CFDワークショップ:GK翼型の空気力学特性解析.ONERA M5全機形態まわりの流れの解析 = Special Publication of National Aerospace Laboratory: Proceedings of the NAL symposium on aircraft computational aerodynamics: CFD workshop on GK airfoil and ONERA M5 geometry. 20:1-55

航空宇宙技術研究所 10-12 Jun. 1992 東京日本
National Aerospace Laboratory 10-12 Jun. 1992 Tokyo Japan
今日、航空機や宇宙機の全機形状まわりのナビエ・ストークス計算が手の届くものとなり、�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::3c45b8c37193a4aaa62159cd412adaa1
http://id.nii.ac.jp/1696/00037729/

Zobrazit plný text záznamu

Wind Tunnel Tests and CFD in Fuji Heavy Industries

Autor: Tanaka, Kohei, Hirose, Hidehiro, Koshioka, Yasuhiro

Publikováno v: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory SP-16. 16:319-326

With the evolution of the CFD technology, the role of wind tunnel has come to be reevaluated. In this paper, the impact of CFD validation with wind tunnel is discussed, that is going to bring the needs for high accuracy of test data, and that will fi

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::583639e7acbcf39c9f394b36126739d0
http://id.nii.ac.jp/1696/00043540/

Zobrazit plný text záznamu

逆解法を用いた翼胴一体化設計について

Autor: Tani, Yosuhiro, Koshioka, Yasuhiro, Hirose, Hidehiro

Publikováno v: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory SP-14. 14:115-120

In this paper, an iterative design procedure is described for three dimensional wing-body configuration, especially blended wing-body configuration, using a three dimensional transonic inverse method with target pressure distribution. In this applica

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::b05864c5b7bf2ffd372175c0a6695a8c
http://id.nii.ac.jp/1696/00043445/

Zobrazit plný text záznamu

二次元剪断流の数値解析

Autor: Koshioka, Yasuhiro

Publikováno v: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory SP-14. 14:197-202

A numerical simulation of the two dimensional (in the sense of mean flow) shear layer is carried out using Arakawa's method. The processes of the growing disturbances and their interactions in the shear layer are simulated clearly. These results show

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::d3fd3d20779458f62addd0809c4cfb5e
http://id.nii.ac.jp/1696/00043458/

Zobrazit plný text záznamu

The CFD Analysis Related Aerospace in Fuji Heavy Industries, Ltd

Autor: Tanaka, Kohei, Hirose, Hidehiro, Koshioka, Yasuhiro

Publikováno v: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory SP-13. 13:57-68

The relations of CFD with design process are discussed. Also, CFD activities in Fuji Heavy Industries, Ltd. are introduced. To obtain full merit of CFD in design, the interactive manner of use is very important. Much more high computing speed is need

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::5f24e56b188801c426073e4d153bb542
http://id.nii.ac.jp/1696/00043421/

Zobrazit plný text záznamu

Vyhledávací nástroje:

Upřesnit hledání