@inproceedings{oai:jaxa.repo.nii.ac.jp:00047339,
 author = {宍戸, 昌子 and SHISHIDO, Masako},
 book = {宇宙航空研究開発機構特別資料: 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2020オンライン論文集, JAXA Special Publication: Proceedings of Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2020 Online},
 month = {Feb},
 note = {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2020オンライン (2020年9月28日-30日. 日本航空宇宙学会 : 宇宙航空研究開発機構(JAXA)オンライン会議), Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2020 Online (September 28-30, 2020. The Japan Society for Aeronautical and Space Sciences : Japan Aerospace Exploration Agency (JAXA), Online meeting), This study proposes a new flow control device (FCD), called one-side FCD or OFCD, to improve conventional cooling hole film effectiveness of turbine airfoils for gas turbine. Detailed numerical investigations on the flat-plate model are executed through RANS (Reynolds-Averaged Navier-Stokes equations) -based simulation using a commercial flow solver, calculating film effectiveness for the type of OFCD. It is found that OFCD performs fairly well., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA2030013018, レポート番号: JAXA-SP-20-008},
 pages = {137--141},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {流れ制御片側デバイスのフィルム冷却向上効果に関する研究},
 volume = {JAXA-SP-20-008},
 year = {2021}
}