@inproceedings{oai:jaxa.repo.nii.ac.jp:00006458,
 author = {Chen, Jinxiang and 小河, 昭紀 and 橋本, 良作 and 吉田, 豊明 and 福山, 佳孝 and Chen, Jinxiang and Ogawa, Akinori and Hashimoto, Ryosaku and Yoshida, Toyoaki and Fukuyama, Yoshitaka},
 book = {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},
 month = {Mar},
 note = {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., 資料番号: AA0048469018, レポート番号: JAXA-SP-04-012},
 pages = {111--116},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {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},
 volume = {JAXA-SP-04-012},
 year = {2005}
}