机译:用层流湍流转换模型在柔性支撑翼型与不可压液流动相互作用中的数值模拟
Czech Tech Univ Fac Mech Engn Ctr Adv Aerosp Technol Dept Tech Math Tech 4 Prague 16607 6 Czech Republic;
Czech Tech Univ Fac Mech Engn Ctr Adv Aerosp Technol Dept Tech Math Tech 4 Prague 16607 6 Czech Republic;
Finite volume method; Arbitrary Lagrangian-Eulerian method; k-k(L)-omega transition model; Aeroelasticity;