机译:旋涡破裂流向俯仰双三角翼的动态响应
School of Aerospace Engineering, Tsinghua University,China Aerodynamics Research and Development Center;
School of Aerospace Engineering, Tsinghua University;
China Aerodynamics Research and Development Center;
China Aerodynamics Research and Development Center;
China Aerodynamics Research and Development Center;
School of Aerospace Engineering, Tsinghua University;
Double-delta wing; Pitching motion; Delayed detached eddy simulation; Reduced frequency; Helical mode instability;
机译:在俯仰双倍倾翼上的非定常涡旋爆发点和动态稳定性的相关性
机译:俯仰双三角翼的涡流特性
机译:超过80º/65º双三角翼的不稳定涡旋破坏的数值研究
机译:基于DDES的投球运动期间,涡流故障流动了双倍角翼
机译:所有国王的马。经历涡旋破坏的三角翼前沿涡旋系统:在动态条件下对其特性和控制的贡献。
机译:机翼-俯仰轴的弦向偏移增强了昆虫机翼上的旋转空气动力:数值研究
机译:80°/ 65°双三角翼非定常涡旋破坏的数值研究
机译:涡街流量计和涡破裂高于三角翼在高亚音速:anExperimental调查(Wervelstroming EN Wervel“击穿”范博文EEN Deltavleugel在Hoog-subsone洛敏:EEN Experimenteel Onderzoek)