School of Aeronautic Science and Engineering, Beihang University, Beijing, China 100191;
School of Aeronautic Science and Engineering, Beihang University, Beijing, China100191;
School of Aeronautic Science and Engineering, BeihangUniversity, Beijing, China 100191;
School of Aeronautic Science and Engineering,Beihang University, Beijing100191;
机译:几何结构非线性对高纵横比机翼颤振和极限循环振荡的影响
机译:基于三阶非线性梁模型的高纵横比机翼颤振分析
机译:柔性高纵横比机翼的非线性气动弹性公式和颤振后分析
机译:高纵横比柔性翼的非线性颤动的参数研究
机译:柔性翼 的 高保真 Aerostructural 优化 与 约束 扑
机译:基于非线性参数模型降阶的直线电机位置检测磁传感器设计与参数研究
机译:具有高纵横比飞机全复合机翼的非线性颤动分析方法研究
机译:纤维取向对高纵横比运输机翼颤振特性影响的实验研究