[American Institute of Aeronautics and Astronautics AIAA Scitech 2020 Forum - Orlando, FL ()] AIAA Scitech 2020 Forum - Blade Element Theory Coupled with CFD Applied to Optimal Design of Rotor for Mars Exploration Helicopter

• 作者Uwatoko, Kazufumi; Kanazaki, Masahiro; Nagai, Hiroki; Fujita, Koji; Oyama, Akira
• 文件大小1096.46KB
• DOI10.2514/6.2020-1284