宇宙航空研究開発機構(JAXA)
宇宙航空研究開発機構(JAXA)
宇宙航空研究開発機構(JAXA)
宇宙航空研究開発機構(JAXA)
German Aerospace Center (DLR)
The French Aerospace Lab (ONERA)
株式会社菱友システムズ
著者所属（英）
Japan Aerospace Exploration Agency (JAXA)
Japan Aerospace Exploration Agency (JAXA)
Japan Aerospace Exploration Agency (JAXA)
Japan Aerospace Exploration Agency (JAXA)
German Aerospace Center (DLR)
The French Aerospace Lab (ONERA)
Ryoyu Systems Co., Ltd.
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)
抄録（英）
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.
内容記述
形態: カラー図版あり
内容記述（英）
Physical characteristics: Original contains color illustrations
Cooperative Research on Rotor Blade Optimization between JAXA-ONERA-DLR: Results of Phase I
AA2030013009.pdf
(2.15MB)
