Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics
Tokyo University of Agriculture and Technology Graduate School of Engineering
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics
出版者
宇宙航空研究開発機構
出版者（英）
Japan Aerospace Exploration Agency (JAXA)
雑誌名
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
雑誌名(英)
JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2004
巻
JAXA-SP-04-012
ページ
111 - 116
発行年
2005-03-25
抄録（英）
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 turbine vane were analyzed based on this interface and the stress evaluation system. As the results, (1) the constructed interface with the quasi-three dimensional interpolation by resolution of plane coordinates and interpolation in two dimensions is of both the simplicity of calculation and wider use, and high precise. (2) In the data processing system, the evaluation parameters were visualized and the distributions corresponding to the multi objectives of stress evaluation were made clear. Thus it is indicated that the present data processing system is effective one for the structural strength database of the virtual turbine.
CFD-構造強度解析におけるデータの受渡し及び処理システムの構築
48469018.pdf
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