@inproceedings{oai:jaxa.repo.nii.ac.jp:00047330,
 author = {木村, 桂大 and 杉浦, 正彦 and 菅原, 瑛明 and 田辺, 安忠 and WILKE, Gunther and BAILLY, Joelle and 竹川, 国之 and KIMURA, Keita and SUGIURA, Masahiko and SUGAWARA, Hideaki and TANABE, Yasutada and WILKE, Gunther and BAILLY, Joelle and TAKEKAWA, Kuniyuki},
 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), A collaborative research on optimization of a main rotor blade for helicopters by JAXA, ONERA and DLR is underway. As a first step, blade optimization method with five design variables is explored by dealing with hovering conditions. Optimizations and simulations are carried out by each agency with their own analysis codes and these results are cross-validated. This paper presents an overview of the project and an interim report on the results obtained so far., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA2030013009, レポート番号: JAXA-SP-20-008},
 pages = {59--67},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {Cooperative Research on Rotor Blade Optimization between JAXA-ONERA-DLR: Results of Phase I},
 volume = {JAXA-SP-20-008},
 year = {2021}
}