Aerodynamic Analysis of NASA-CRM at Low Speed and High Angle of Attack conditions Using Hierarchical Cartesian Mesh and Immersed Boundary Method

原 惇, 菅谷 圭祐, Atsushi HARA, SUGAYA Keisuke, IMAMURA Taro
doi:10.20637/00048018 fatcat:ymyes6nccfcrpkf3xiipqoodre