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of 34
pro vyhledávání: '"YOSHIDA, Toyoaki"'
Publikováno v:
大原社会問題研究所雑誌 = The Journal of Ohara Institute for Social Research. 578:58-61
Autor:
SAEKI, Hiroshi, MATSUSHITA, Masahiro, FUKUYAMA, Yoshitaka, YOSHIDA, Toyoaki, YOKOKAWA, Tadaharu, HARADA, Hiroshi
Publikováno v:
日本ガスタービン学会誌 = Journal of the Gas Turbine Society of Japan. 36(4):283-288
資料番号: PA0810085000
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
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
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
Akademický článek
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Autor:
YOSHIDA, TOYOAKI
Publikováno v:
Annals of the New York Academy of Sciences; 2001, Vol. 934 Issue 1, p194-205, 12p
Autor:
Yoshida, Makoto1 (AUTHOR), Sawano, Toyoaki2,3,4 (AUTHOR) toyoakisawano@gmail.com, Kobashi, Yurie4,5 (AUTHOR), Hori, Arinobu6 (AUTHOR), Nishikawa, Yoshitaka5 (AUTHOR), Ozaki, Akihiko7 (AUTHOR), Nonaka, Saori3 (AUTHOR), Tsuboi, Motohiro8,9 (AUTHOR), Tsubokura, Masaharu3,4,5 (AUTHOR)
Publikováno v:
Journal of Medical Case Reports. 2/7/2023, Vol. 17 Issue 1, p1-6. 6p.
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
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
レポート番号: NAL TR-427