@inproceedings{oai:jaxa.repo.nii.ac.jp:00004757,
 author = {吉新, 哲也 and 佐々木, 大輔 and 中橋, 和博 and Yoshiara, Tetsuya and Sasaki, Daisuke and Nakahashi, Kazuhiro},
 book = {宇宙航空研究開発機構特別資料: 第42回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2010 論文集, JAXA Special Publication: Proceedings of 42nd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2010},
 month = {Feb},
 note = {第42回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2010 (2010年6月24日-25日. 米子コンベンションセンター BiG SHiP), 42nd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2010 (June 24-25,  2010. Yonago Convention Center BiG SHiP), Yonago, Tottori Japan, Conjugate heat transfer method was implemented in the unstructured-mesh CFD solver to predict the thermal loads of the two- and three-dimensional cooled turbine blades. In this simulation, the fluid domain and the solid domain are solved simultaneously satisfying the equality of the heat flux and wall temperature on the boundary of the fluid and solid. The results of the surface temperature and the external heat transfer coefficient distributions are in close agreement with the experimental data especially in the two-dimensional calculation., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0064967050, レポート番号: JAXA-SP-10-012},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {非構造格子CFDソルバーによる内部対流冷却翼列の流体・熱伝導連成数値計算},
 volume = {JAXA-SP-10-012},
 year = {2011}
}