@inproceedings{oai:jaxa.repo.nii.ac.jp:00006635,
 author = {山根, 敬 and 山本, 一臣 and 吉田, 豊明 and Yamane, Takashi and Yamamoto, Kazuomi and Yoshida, Toyoaki},
 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2003論文集, JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2003},
 month = {Mar},
 note = {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 flow simulation and heat conduction calculation which is a severe problem in coupled simulation has been overcome by incorporating a heat conduction sub-step method. The developed program has been applied to simulations of a turbine cooling structure which are the integration of impingement and pin cooling device., 資料番号: AA0047427034, レポート番号: JAXA-SP-03-002},
 pages = {190--195},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {タービン翼の流体・熱伝導連成解析},
 volume = {JAXA-SP-03-002},
 year = {2004}
}