Výsledky vyhledávání - "YOSHIDA, Toyoaki"

Construction of delivery of the data in CFD-structural strength analysis and processing system

Autor: Chen, Jinxiang, Ogawa, Akinori, Hashimoto, Ryosaku, Yoshida, Toyoaki, Fukuyama, Yoshitaka

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. :111-116

In order to construct a database of structural strength for a virtual turbine made of single crystal Ni-base superalloy, an interface and a stress evaluation system were proposed. Then the thermal stress and its properties of the 1,400 C virtual turb

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::95dac7e694b75e8931fc6a0f66ee66da
http://id.nii.ac.jp/1696/00006452/

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タービン翼の流体・熱伝導連成解析

Autor: Yamane, Takashi, Yamamoto, Kazuomi, Yoshida, Toyoaki

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2003論文集 = JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2003. :190-195

A new coupled simulation program for flow and heat conduction has been developed based upon a common CFD platform UPACS. It connects flow calculation blocks and solid blocks without using surface temperature values explicitly. The time-lag between fl

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::868fe40ffdb7674a3c80ff10f14782c0
http://id.nii.ac.jp/1696/00006629/

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Fundamental evaluation of functionally gradient materials in the simulation of a high-temperature, high-speed rotating field. Part 1: Evaluation tests of stepwise graded material

Autor: Fujisawa, Yoshiaki, Taki, Masanobu, Sofue, Yasushi, Yoshida, Toyoaki

Publikováno v: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory. 1209:1-12

熱応力緩和型傾斜機能材料など耐熱材料をガスタービンのタービンブレードなどの高応力環境に適用する際には、熱応力(温度落差)と機械的応力(回転部材の場合、特に遠心力による引張�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::96d2454e20f1534f863bae6c918983e5
http://id.nii.ac.jp/1696/00041188/

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Akademický článek

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Akademický článek

Cooling Systems for Ultra-High Temperature Turbines.

Autor: YOSHIDA, TOYOAKI

Publikováno v: Annals of the New York Academy of Sciences; 2001, Vol. 934 Issue 1, p194-205, 12p

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Analysis of Temperature Distribution and Thermal Stress by The Finite Element Method and Application to Turbine Blade and Disk

Autor: MATSUSUE, Katsutoshi, YOSHIDA, Toyoaki, HASHIMOTO, Ryosaku, OGAWA, Akinori, ISOBE, Toshio

Publikováno v: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-481. 481:24

The location and configuration effects of cooling passages, in an air-cooled turbine blade, on blade thermal transient stress under engine operating conditions were investigated using a finite-element Fortran program written to provide a solution to

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::255089059a38045046d72639ef9a4b48
http://id.nii.ac.jp/1696/00044728/

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New Molding Method at Three-Dimensional Hollow Photoelastic Model and Centrifugal Stress Analyses of Air-Cooled Turbine Blades

Autor: YOSHIDA, Toyoaki, MATSUSUE, Katsutoshi, TAKAHARA, Kitao, HASHIMOTO, Ryosaku

Publikováno v: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-427. 427:14

資料番号: NALTR0427000
レポート番号: NAL TR-427

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::9d6ed286e74e1d4825c2ad7dfccb7035
http://id.nii.ac.jp/1696/00044670/

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New Molding Method of Three-Dimensional Hollow Photoelastic Model and Centrifugal Stress Analysis of Air Cooled Turbine Blade Model

Autor: YOSHIDA, Toyoaki, MATSUSUE, Katsutoshi, TAKAHARA, Kitao, HASHIMOTO, Ryosaku

Publikováno v: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-427T. :16

中空部のある三次元物体の光弾性模型を製作する新しい方法を考案し，冷却タービン動翼模型に適用して，遠心応力の解析を行った。製作法の特長は複雑な中空形状を成形するための中�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::4ed563f172a6764f376f4900335d0def
http://id.nii.ac.jp/1696/00044671/

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赤外線温度計測装置(Ⅱ)ソフトウェア

Autor: YOSHIDA, Toyoaki

Publikováno v: 航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory. 531:53

資料番号: NALTM0531000
レポート番号: NAL TM-531

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::b80211207be9912846287453f2c85c6e
http://id.nii.ac.jp/1696/00044108/

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